2002 - Satlist
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Year of Launch 2002 Name [Launcher] Fragment $ Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Orbital Inclination (deg) Size (m) Lifetime Date of orbital determination Nodal period (min) Page 2002 -1 Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) Milstar 5 (USA 164) [Titan 4B] 2002 01 A [27168] CC 2002 Jan 16.02 > million years No TLE issued Titan 4B 3rd stage (Centaur) 2002 01 B [27169] 2002 Jan 16.02 No TLE issued. Orbits from visual observations. 2009 Mar 9.88 1.79 1437.75 42197 35593 36044 0.005 45 Insat 3C [Ariane-42L] (V147 #108) 2002 02 A [27298] KOU-ELA2 2002 Jan 23.99 > million years Box+ 2 panels 2750 1050 dry 1.7x2.0 x2.8 15.4 span 2002 2002 2002 2002 2002 2002 2002 2002 2002 2010 2010 2010 2011 24.67 25.86 27.17 28.37 30.24 4.96 6.62 7.80 11.66 15.64 19.14 3.69 29.70 4.01 1.71 0.82 0.17 0.17 0.21 0.18 0.16 0.17 0.12 0.17 0.04 0.02 638.70 817.02 1114.32 1351.53 1428.80 1432.90 1433.83 1435.78 1436.10 1436.08 1450.67 1436.10 1436.08 24563 28950 33441 40493 42022 42102 42120 42159 42165 42164 42449 42165 42165 580 9363 18355 32447 35505 35444 35652 35758 35775 35769 36065 35768 35781 35790 35780 35770 35782 35782 36003 35831 35802 35798 35803 36077 35804 35791 0.717 0.456 0.260 0.041 0.003 0.007 0.002 0.0005 0.0003 0.0004 0.0001 0.0004 0.0001 179 178 177 170 175 146 144 172 48 28 250 16 147 Ariane-4 3rd stage (H-10-3) +VEB 2002 02 B [27299] 2002 Jan 23.99 Cylinder 1250 + 250 Cylinder 11.05 long 2.6 dia 1.03x4.0 2002 Jan 24.70 2012 Jan 5.08 3.98 4.37 656.05 653.70 25011 24951 425 476 36839 36668 0.728 0.725 178 54 Tsubasa (MDS-1) [H-2A] 2002 03 A [27367] TAN 2002 Feb 4.11 2002 Feb 4.80 2012 Jan 3.89 28.55 28.51 635.52 619.72 24486 17370 480 219 35734 21764 0.720 0.620 179 154 DASH + VEP 3 2002 03 B [27368] 2002 Feb 4.11 2002 Feb 4.80 2012 Jan 4.39 28.53 29.06 634.73 625.75 24466 24234 486 405 35688 35306 0.719 0.720 179 93 H-2A 2nd stage 2002 03 C [27369] 2002 Feb 4.11 2002 2004 2004 2004 2012 4.80 3.45 6.70 6.86 2.60 28.74 28.71 24.36 23.81 23.80 635.88 626.18 607.12 607.10 607.10 24495 24246 23751 23750 23750 482 442 1046 992 1054 35752 35292 33698 33751 33689 0.720 0.719 0.687 0.690 0.687 179$ 288$ 278 41 88 DASH + VEP 3 Shroud half 2002 03 D [28237] 2002 Feb 4.11 2004 May 7.36 2012 Jan 5.17 28.71 29.05 626.18 616.48 24245 23994 443 403 35291 34829 0.719 0.717 290 122 DASH + VEP 3 Shroud half 2002 03 E [28243] 2002 Feb 4.11 2004 May 6.40 2012 Jan 4.42 28.73 29.04 629.23 618.07 24324 24036 445 401 35447 34913 0.719 0.718 287 107 Probably these orbits belong to one of the shroud halves, 2002 03 D or E. 2014-version 1.13 Jan Jan Jan Jan Jan Feb Feb Feb Feb Nov Nov Dec Dec Feb May May Dec Jan Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] HESSI [L1011/Pegasus-XL] D RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Date of orbital determination Orbital Inclination (deg) Size (m) Lifetime Nodal period (min) Page 2002 -2 Semi major axis (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) 6977 6929 588 540 609 561 0.002 0.002 276 340 6975 6948 583 561 609 578 0.002 0.001 274 186 2002 04 A [27370] CC 2002 Feb 5.87 2002 Feb 5.87 2012 Jan 3.71 38.04 38.04 Pegasus-XL 3rd stage 2002 04 B [27371] 2002 Feb 5.87 2002 Feb 5.87 2012 Jan 5.01 38.04 38.03 Iridium 91 [Delta-2 (7920)] 2002 05 A [27372] VDB 2002 Feb 11.74 Box+ 2 panels 657 full 556 empty 1 across 3.5 long 2002 2002 2009 2009 2009 2012 Feb Feb Feb Feb Mar Jan 11.78 21.54 27.16 27.23 2.09 4.45 86.58 86.58 86.58 86.54 86.40 86.39 97.35 98.18 98.18 98.58 100.40 100.40 7010 7050 7050 7070 7156 7156 623 659 667 683 773 776 641 683 676 699 781 778 0.001 0.002 0.0006 0.001 0.0005 0.0001 241 211 56 16 74 272 Iridium 90 2002 05 B [27373] 2002 Feb 11.74 Box+ 2 panels 657 full 556 empty 1 across 3.5 long 2002 2002 2005 2006 2008 2012 Feb Feb Oct Aug Jan Jan 11.78 21.47 13.49 19.98 22.77 4.46 86.58 86.58 87.08 87.10 86.45 86.45 97.35 98.18 99.77 99.78 99.78 99.78 7010 7050 7126 7127 7127 7127 623 664 743 745 747 744 641 679 753 752 750 753 0.001 0.001 0.0007 0.0005 0.0002 0.0006 241 197 131 144 218 131 Iridium 94 2002 05 C [27374] 2002 Feb 11.74 Box+ 2 panels 657 full 556 empty 1 across 3.5 long 2002 2002 2002 2012 Feb Feb Feb Jan 11.78 11.95 19.23 1.14 86.58 86.58 86.58 85.94 97.35 97.40 98.18 98.20 7010 7013 7050 7051 623 627 666 669 641 641 677 676 0.001 0.001 0.0008 0.0005 241 231 202 207 Iridium 95 2002 05 D [27375] 2002 Feb 11.74 Box+ 2 panels 657 full 556 empty 1 across 3.5 long 2002 2002 2002 2008 2012 Feb Feb Feb Jul Jan 11.78 11.94 22.85 25.98 3.93 86.58 86.58 86.58 86.39 86.40 97.35 97.42 98.18 100.40 100.40 7010 7014 7050 7156 7156 623 628 664 774 775 641 642 679 780 779 0.001 0.001 0.001 0.0004 0.0002 241 217 203 88 89 Iridium 96 2002 05 E [27376] 2002 Feb 11.74 Box+ 2 panels 657 full 556 empty 1 across 3.5 long 2002 2002 2002 2012 Feb Feb Feb Jan 11.78 11.94 17.47 4.41 86.58 86.58 86.58 86.58 97.35 97.37 98.17 98.20 7010 7011 7050 7051 623 625 664 671 641 641 678 674 0.001 0.001 0.001 0.0002 241 231 179 88 Delta-2 2nd stage 2002 05 F [27377] 2002 Feb 11.74 217 days 2002 Sep 16 Cylinder 919 5.88 long 2.44 dia 2002 2002 2002 2002 Feb Feb Feb Sep 11.78 12.06 12.24 16.74 86.58 86.58 84.43 84.38 97.35 97.38 94.02 87.52 7010 7012 6849 6530 623 626 312 137 641 640 630 166 0.001 0.001 0.023 0.002 241 237 352 255 Fragments Iridium 91 2002 05 G-K 2014-version 1.13 4 pieces, all in orbit 96.65 95.67 Perigee height (km) 96.60 96.05 For orbital information see extra pages at end of year Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Date of orbital determination Orbital Inclination (deg) Size (m) Lifetime Page 2002 -3 Nodal period (min) Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) Echostar 7 [Atlas 3B] 2002 06 A [27378] CC 2002 Feb 21.53 > million years 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2012 Feb Feb Feb Feb Mar Mar Mar Mar Mar Mar Mar Jan 21.20 23.78 26.62 28.37 4.77 6.90 7.00 8.01 9.13 11.70 15.13 4.26 22.59 16.95 10.74 5.08 0.50 0.21 0.85 0.07 0.06 0.03 0.06 0.02 1085.83 1146.95 1221.57 1516.13 1638.20 1438.43 1526.48 1439.18 1438.17 1436.13 1436.07 1436.07 34995 36296 38676 43717 46034 42211 43916 42225 42205 42165 42164 42164 232 2782 7593 17700 35741 35734 35771 35742 35742 35779 35779 35776 57001 57053 57001 56977 43568 35930 39304 35952 35912 35794 35793 35796 0.811 0.748 0.639 0.449 0.085 0.002 0.040 0.002 0.002 0.002 0.0002 0.0002 177 179 180 179 173 345 355 62 46 78 6 26 Atlas 3B 2nd stage (Centaur) 2002 06 B [27379] 2002 Feb 21.53 215.2 days 2002 Sep 24.7 2002 2002 2002 2002 2002 Feb Sep Sep Sep Sep 21.19 16.50 21.74 24.57 24.67 23.37 22.62 22.53 22.53 22.60 1085.27 899.88 501.75 123.07 101.82 34983 30876 20917 8196 7223 211 127 109 99 75 56997 48868 28967 3535 1614 0.811 0.789 0.690 0.210 0.107 180 256 259 266 262 Intelsat 904 [Ariane-44L] (V148) 2002 07 A [27380] KOU-ELA2 2002 Feb 23.29 > million years Box+ 2 panels 4680 2350 dry 2.80x3.50 x5.56 31 span 2002 2002 2002 2002 2002 2002 2002 2012 Feb Feb Feb Feb Mar Mar Apr Jan 23.09 24.40 27.12 27.78 7.75 12.69 2.68 4.68 6.96 3.83 0.56 0.24 0.05 0.06 0.05 0.01 631.43 736.50 1146.75 1293.03 1436.13 1436.03 1436.07 1436.10 24381 27015 36292 39316 42166 42164 42164 42165 182 5475 24053 30096 35783 35778 35782 35773 35822 35799 35774 35778 35791 35791 35789 35799 0.731 0.561 0.161 0.072 0.00009 0.0002 0.00007 0.0003 178 179 183 194 52 2 219 276 D Ariane-4 3rd stage (H-10-3)+VEB 2002 07 B [27381] 2002 Feb 23.29 128 days 2002 Jul 1 Cylinder 1250 + 520 Cylinder 11.05 long 2.6 dia 1.03x4.0 2002 Feb 23.09 2002 Jul 1.13 6.99 6.99 660.98 93.47 25135 6823 198 107 37316 781 0.738 0.049 178 134 D Cosmos 2387 [Soyuz-U] 2002 08 A [27382] PLE 2002 Feb 25.73 122 days 2002 Jun 27 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 67.13 67.12 67.12 67.12 67.13 67.11 67.11 67.11 67.10 67.10 67.10 67.10 67.10 89.63 89.43 89.95 89.52 90.03 89.10 89.72 89.08 90.38 89.65 90.37 89.58 90.02 6635 6625 6650 6629 6655 6609 6639 6608 6672 6635 6671 6632 6654 165 163 184 176 224 198 205 189 247 229 232 213 200 348 331 359 325 328 262 316 269 339 285 352 294 351 0.014 0.013 0.013 0.011 0.008 0.005 0.008 0.006 0.007 0.004 0.009 0.006 0.011 95 93 73 70 79 59 86 76 172 149 128 101 96 D 2002 08 continued on next page 2014-version 1.13 Feb Feb Feb Mar Mar Mar Mar Apr Apr Apr Apr May May 25.78 27.96 28.22 5.63 5.82 23.95 24.08 2.28 2.58 27.55 27.67 23.13 23.36 Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Date of orbital determination Orbital Inclination (deg) 2002 2002 2002 2002 2002 3.89 4.21 15.99 16.05 26.80 67.10 67.10 67.09 67.09 67.09 89.48 90.02 89.33 89.85 89.15 2002 Feb 25.78 2002 Feb 28.46 67.11 67.11 89.60 88.22 Size (m) Lifetime Jun Jun Jun Jun Jun Nodal period (min) Page 2002 -4 Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) 6627 6654 6620 6646 6611 189 192 181 181 168 308 358 302 353 297 0.009 0.013 0.009 0.013 0.010 84 95 83 82 69 6633 6565 165 141 344 232 0.013 0.007 95 89 88.70 6589 87.50 6529 162 143 259 159 0.007 0.001 68 313 7154 7162 7166 7163 7162 7155 7153 7145 7145 766 783 785 784 783 774 773 765 766 784 784 789 784 784 779 775 768 767 0.001 0.0001 0.0003 0 0.0001 0.0004 0.0001 0.0002 0.0001 262 10 72 145 92 283 101 52 86 100.53 7163 100.30 7152 783 750 785 796 0.0001 0.003 36 322 D Soyuz U 3rd stage (Block I) 2002 08 B [27383] 2002 Feb 25.73 3 days 2002 Feb 28 D Fragment 2002 08 C [27456] 2002 Jun 28 123 days 2002 Jun 27.29 2002 Jun 27.46 67.09 67.09 Envisat [Ariane-5] (V145 #511) 2002 09 A [27386] KOU-ELA3 2002 Mar 1.05 Box + panel 8111 4x4x10 26 span 2002 2002 2002 2002 2010 2010 2010 2010 2012 98.53 98.54 98.55 98.56 98.54 98.55 98.54 98.54 98.48 Ariane-5 2nd stage (EPS)+VEB 2002 09 B [27387] 2002 Mar 1.05 Drum-cone 1190 + 1500 Cylinder 3.36 long 3.94 dia 1.56x4.56 2002 Mar 1.19 2012 Jan 6.92 98.54 98.20 D STS-102 # 7M Discovery F29 R [Shuttle] 2002 10 A [27388] CC-LC39A 2002 Mar 1.47 10.93 days 2002 Mar 12.40 Delta wing 116989 ↑ 100564 ↓ 37.5 long 5.5 dia 23.8 span 2002 2002 2002 2002 2002 2002 2002 2002 Mar Mar Mar Mar Mar Mar Mar Mar 1.51 1.92 2.23 3.58 8.78 9.51 11.47 12.25 28.46 28.46 28.47 28.47 28.47 28.47 28.67 28.47 92.28 92.40 92.43 96.17 96.28 95.40 95.27 95.27 6765 6771 6772 6953 6959 6917 6910 6910 199 211 213 566 578 498 485 485 574 574 574 583 584 578 577 577 0.028 0.027 0.027 0.001 0.0004 0.006 0.007 0.007 52 57 60 158 201 48 67 76 TDRS 9 * [Atlas-2A] (AC-143) 2002 11 A [27389] CC-LC36A 2002 Mar 8.96 > million years Box + 2 panels + 2 dishes 3180 21 span 1777 bol 5 dia dish 2002 2002 2002 2002 2002 Mar Mar Mar Mar Mar 9.52 11.64 13.71 19.95 26.00 27.14 26.39 26.31 21.37 17.36 507.28 566.80 635.78 696.73 797.02 21070 22687 24493 26034 28476 248 439 429 3521 8383 29135 32178 35800 35789 35811 0.686 0.700 0.722 0.620 0.482 177 178 179 183 185 Mar Mar Mar Mar Oct Oct Oct Oct Jan 1.12 2.45 3.96 4.11 22.13 22.42 23.18 26.82 7.21 100.35 100.53 100.60 100.55 100.53 100.38 100.33 100.17 100.17 2002 11 continued on next page # * Crew of 7 astronauts (Altman, Carey, Grunsfield, Currie, Newman, Linnehan and Massimino) performed the 4th service mission to the Hubble Space Telescope. Hubble was grappled by the shuttle robot arm and 2002 Mar 3.438 placed in the cargobay. After 5 spacewalks Hubble was released 2002 Mar 9.420. Malfunction of the helium pressurization tank #2 prevented the use of the 2nd fuel tank. Engineers found a solution to use the #1 helium tank. In 2011 Aug-Oct TDRS 9 was moved from ° to 40.90°W 2014-version 1.13 Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Date of orbital determination Orbital Inclination (deg) 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2011 2011 2011 2011 2011 2011 2011 Size (m) Lifetime Jun Jun Jul Aug Sep Sep Sep Oct Oct Oct Nov Aug Aug Aug Aug Sep Sep Oct 13.40 19.69 17.83 11.74 12.44 23.36 24.79 2.30 5.26 15.48 14.38 4.18 4.36 8.90 10.29 3.97 29.21 13.25 Page 2002 -5 Nodal period (min) Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) 16.53 16.37 15.71 14.81 13.72 11.36 10.02 8.51 8.50 8.42 8.35 1.40 1.40 1.41 1.40 1.43 1.41 1.42 815.47 829.48 589.02 903.98 976.25 1098.48 1279.87 1438.15 1436.55 1436.23 1436.08 1436.20 1434.75 1434.22 1433.15 1435.37 1436.05 1436.08 28914 29244 29934 30947 32599 35266 39049 42205 42174 42167 42165 42167 42139 42128 42107 42151 42164 42165 9254 9947 11286 13301 16632 22006 29507 35795 35778 35754 35763 35721 35710 35699 35659 35709 35733 35736 35816 35783 35824 35835 35808 35769 35833 35858 35813 35824 35809 35856 35809 35799 35798 35835 35838 35836 0.459 0.441 0.410 0.364 0.294 0.195 0.081 0.0007 0.0004 0.0008 0.0006 0.002 0.001 0.001 0.002 0.001 0.001 0.001 198 199 203 208 214 222 219 327 3 31 35 228 250 239 229 225 227 227 Atlas-2A 2nd stage Centaur 2002 11 B [27390] 2002 Mar 8.96 2002 Mar 9.51 2012 Jan 5.44 27.03 26.76 506.22 392.27 21040 17751 233 230 29091 22514 0.686 0.628 177 87 Grace 1 [Rokot/Breeze-KM] 2002 12 A [27391] PLE 2002 Mar 17.39 2002 Mar 17.44 2012 Jan 5.76 89.01 89.00 94.52 93.63 6873 6830 484 440 505 464 0.002 0.002 265 75 Grace 2 2002 12 B [27392] 2002 Mar 17.39 2002 Mar 17.71 2012 Jan 5.76 89.05 89.01 94.52 93.63 6874 6830 483 439 507 465 0.002 0.002 281 77 D Breeze-KM stage 2002 12 C [27393] 2002 Mar 17.39 10 days 2002 Mar 27 2002 Mar 17.76 2002 Mar 27.22 89.01 88.99 90.98 87.20 6702 6514 142 102 504 170 0.027 0.005 261 240 D Progress-M1 8 * [Soyuz-U] 2002 13 A [27395] BAI-LC1 2002 Mar 21.84 96 days 2002 Jun 25 Cyl+ 2 panels+ 7.9 long 2002 Mar 21.90 beehive+sphere 2.12 maxdia 2002 Mar 22.22 7265 2002 Mar 22.98 2002 Mar 23.11 2002 Mar 23.99 2002 Mar 25.18 2002 Apr 14.81 2002 Apr 15.83 2002 Apr 17.58 2002 Jun 11.81 51.52 51.64 51.64 51.63 51.64 51.63 51.63 51.64 51.64 51.64 6589 6677 6685 6693 6697 6770 6765 6766 6773 6765 188 284 283 284 295 388 384 384 388 382 233 313 330 346 342 394 388 391 400 390 0.003 0.002 0.003 0.005 0.004 0.0004 0.0003 0.0005 0.0008 0.0006 92 71 86 80 84 315 20 2 346 187 2002 13 continued on next page. * Docked with ISS (Zvevda aft port) 2002 Mar 24.873; undocked 2002 Jun 25.351. 2014-version 1.13 88.72 90.48 90.65 90.82 90.88 92.38 92.28 92.30 92.43 92.28 Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Date of orbital determination Orbital Inclination (deg) 2002 Jun 14.88 2002 Jun 23.80 2002 Jun 25.48 51.64 51.64 51.64 2002 Mar 22.02 2002 Mar 23.49 51.61 51.61 Cylinder 2400? Size (m) Lifetime 8.1 long 2.66 dia Nodal period (min) Page 2002 -6 Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) 92.43 6773 92.42 6771 92.32 6767 389 388 379 399 398 398 0.0007 0.0007 0.001 236 273 290 88.62 6584 87.27 6518 185 133 227 145 0.003 0.001 93 94 D Soyuz-U 3rd stage (Block I) 2002 13 B [27396] 2002 Mar 21.84 1.8 days 2002 Mar 23.6 D R Shen Zhou 3 $ [CZ-2F] 2002 14 A [27397] JIUQ 2002 Mar 25.59 6.78 day 2002 Apr 1.37 2002 Mar 26.08 2002 Apr 1.47 42.40 42.41 91.22 91.22 6713 6712 332 329 337 338 0.0004 0.0007 272 327 D CZ-2F 2nd stage 2002 14 B [27398] 2002 Mar 25.59 8.4 days 2002 Apr 3.0 2002 Mar 26.08 2002 Apr 2.92 42.40 42.39 89.73 87.23 6640 6516 197 120 326 155 0.010 0.003 132 67 D Orbital module * 2002 14 C [27408] 2002 Mar 25.59 231.69 days 2002 Nov 12.28 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 Apr Apr Apr Apr Apr Jun Jun Jul Jul Nov 1.44 1.74 1.87 24.89 25.25 13.67 14.24 16.18 17.85 12.00 42.41 42.42 42.40 42.40 42.41 42.41 42.40 42.40 42.41 42.40 91.22 91.58 92.63 91.08 92.25 91.78 92.15 91.98 92.13 87.82 6713 6731 6734 6706 6763 6741 6758 6751 6758 6545 330 349 353 324 382 355 374 370 376 164 339 355 357 331 388 369 385 374 382 169 0.0007 0.0004 0.0003 0.0005 0.0004 0.001 0.0008 0.0003 0.0004 0.0004 322 254 262 45 51 32 282 194 213 269 JCSat 8 [Ariane-44L] (V149 #110) 2002 15 A [27399] KOU-ELA2 2002 Mar 29.06 > million years Box+ 2 panels 2600 2.7x3.6 x4.3 21 span 2002 2002 2002 2002 2002 2002 2012 Mar Apr Apr Apr Apr Apr Jan 29.30 1.90 7.21 17.16 25.52 29.59 4.50 3.97 0.65 0.02 0.01 0.02 0.02 0.04 632.73 1111.78 1435.93 1436.08 1432.22 1436.10 1436.08 24414 35550 42162 42165 42089 42165 42165 355 22596 35779 35782 35697 35780 35778 35716 35747 35787 35790 35723 35793 35794 0.724 0.185 0.0001 0.00009 0.0003 0.0002 0.0002 175 182 125 317 351 240 66 Astra 3A 2002 15 B [27400] 2002 Mar 29.06 > million years Cylinder 1495 7.97 high 2.17 dia 2002 2002 2002 2012 2013 2013 2013 Mar Apr Apr Jan Oct Oct Oct 29.30 3.70 12.53 7.01 13.01 16.00 18.78 4.04 0.04 0.02 0.03 1.17 1.16 1.19 635.15 1380.90 1435.98 1436.05 1436.07 1446.15 1448.62 24477 41077 42163 42164 42164 42361 42410 273 33626 35762 35762 35768 35954 35976 35922 35771 35806 35808 35803 36012 36086 0.728 0.026 0.0005 0.0005 0.0004 0.0007 0.001 178 150 231 342 164 218 216 2002 Mar 29.31 2012 Jan 6.04 4.05 3.73 631.33 444.55 24378 19295 258 236 35741 25597 0.728 0.657 176 22 Graveyard orbit Ariane-4 3rd stage (H-10-3) +VEB 2014-version 1.13 2002 15 C [27401] 2002 Mar 29.06 Cylinder 1670 + 520 Cylinder 11.05 long 2.6 dia 1.03x4.0 Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Date of orbital determination Orbital Inclination (deg) Size (m) Lifetime Nodal period (min) Page 2002 -7 Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) Spelda upperpart 2002 15 D [27402] 2002 Mar 29.06 2002 Mar 30.62 2012 Jan 6.21 4.04 3.69 636.02 594.88 24499 23431 296 300 35945 33804 0.728 0.715 177 350 Intelsat 903 [Proton-K] 2002 16 A [27403] BAI 2002 Mar 30.73 > million years 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2012 30.78 31.22 3.50 5.90 11.31 17.19 22.86 16.28 22.30 23.43 26.63 5.08 51.67 25.08 11.02 0.69 0.10 0.08 0.07 0.02 0.02 0.00 0.01 0.02 631.85 697.72 850.75 1332.60 1435.98 1436.08 1436.10 1440.55 1435.95 1436.07 1436.10 1436.10 24366 26059 29742 40114 42163 42165 42165 42252 42162 42164 42165 42165 153 3474 10886 31653 35772 35775 35775 35828 35777 35780 35780 35774 35821 35886 35841 35817 35797 35797 35798 35919 35790 35792 35793 35799 0.732 0.622 0.420 0.052 0.0003 0.0003 0.0003 0.001 0.0002 0.0001 0.0001 0.0003 359 359 0 0 175 161 164 198 126 4 119 159 Proton-K 4th stage (Block DM3) 2002 16 B [27404] 2002 Mar 30.73 2002 Mar 31.24 2012 Jan 6.54 25.01 24.55 698.00 698.03 26065 26067 3461 3619 35912 35756 0.622 0.616 358 357 D Cosmos 2388 [Molniya-M] 2002 17 A [27409] PLE 2002 Apr 1.92 3453 days 2011 Sep 14 2002 2002 2011 2011 18.22 23.12 13.47 14.28 62.93 62.92 65.42 64.76 715.60 718.10 715.82 88.20 26502 26563 26507 6564 519 516 253 58 39727 39854 40005 313 0.740 0.740 0.750 0.019 287 287 228 241 D Molniya-M 3rd stage 2002 17 B (Block I) [27410] 2002 Apr 1.92 28.5 days 2002 Apr 29.4 2002 Apr 4.01 2002 Apr 29.16 62.83 62.80 91.77 6740 87.63 6536 231 143 490 170 0.019 0.002 113 121 D Molniya-M 4th stage casing 2002 17 C [27411] 2002 Apr 1.92 16.9 days 2002 Apr 18.8 2002 Apr 4.01 2002 Apr 18.76 62.86 62.73 91.58 6731 87.72 6540 197 -18 508 341 0.023 0.027 116 333 Molniya-M 4th stage (Block ML) 2002 17 D [27412] 2002 Apr 1.92 4644 days 2014 Dec 18 Cylinder 900 2.3 long 2.2 dia 2002 2002 2012 2014 Apr Apr Jan Dec 1.92 19.03 7.10 17.97 62.89 62.89 63.76 62.19 6801 26171 26089 6593 192 517 240 89 653 39069 39181 340 0.034 0.737 0.746 0.019 117 287 249 269 2002 18 A [27413] CC-LC39 2002 Apr 8.864 10.822 days 2002 Apr 19.686 Delta wing 257079 ↑ 200657 ↓ 37.5 long 5.5 dia 23.8 span 2002 2002 2002 2002 2002 2002 2002 Apr Apr Apr Apr Apr Apr Apr 8.89 10.68 15.07 17.96 18.52 18.78 19.25 51.64 51.64 51.64 51.64 51.64 51.64 51.63 6571 6765 6766 6771 6771 6732 6733 155 384 385 385 385 308 308 230 388 390 399 399 399 401 0.006 0.0003 0.0004 0.001 0.001 0.007 0.007 344 8 358 342 348 14 18 D D STS-110 # 7M Atlantis F25 R [Shuttle] * # Cylinder 1976 8.1 long 2.66 dia 300? Mar Mar Apr Apr Apr Apr Apr May May May May Jan Apr Apr Jan Sep 93.02 702.25 698.95 88.78 88.33 92.28 92.32 92.40 92.40 91.60 91.63 Orbital module separated from Shenzhou capsule and service module 2002 Apr 1. Crew of 7 astronauts (Bloomfield, Frick, Ross, Smith, Ochoa, Morin and Walheim) docked with ISS ( PMA-2/Destiny port) 2002 Apr 10.670; undocked 2002 2014-version 1.13 Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Orbital Inclination (deg) Apr 18.772. Installed the S0 truss and mobile transporter. 2014-version 1.13 Size (m) Lifetime Date of orbital determination Nodal period (min) Page 2002 -8 Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Size (m) Lifetime Date of orbital determination Orbital Inclination (deg) Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) NSS 7 [Ariane-44L] (V150 #111) 2002 19 A [27414] KOU-ELA2 2002 Apr 16.96 > million years Box+ 2 panels 4700 3.62x3.62 x6.7 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2012 16.76 21.52 21.77 23.52 29.51 1.01 23.34 24.70 24.90 28.38 4.04 7.31 7.03 4.36 1.73 0.71 0.04 0.02 0.01 0.05 0.01 0.04 0.06 0.02 630.78 748.33 938.53 1149.48 1436.05 1436.08 1436.10 1434.78 1433.63 1436.12 1436.08 1436.10 24364 27304 31754 36350 42164 42165 42165 42139 42117 42165 42164 42165 221 6647 15047 34200 35778 35776 35779 35737 35700 35779 35779 35774 35750 35204 35703 35742 35793 35796 35793 35784 35776 35795 35793 35799 0.729 0.523 0.325 0.159 0.0002 0.0002 0.0002 0.0006 0.0009 0.0002 0.0002 0.0003 178 182 180 181 88 81 239 288 263 258 272 280 Ariane-4 3rd stage (H-10-3)+VEB 2002 19 B [27415] 2002 Apr 16.96 1075 days 2005 Mar 26 Cylinder 1670 + 520 Cylinder 11.05 long 2.6 dia 1.03x4.0 2002 Apr 16.75 2005 Mar 26.28 7.00 6.45 661.25 90.68 25142 6687 248 106 37279 510 0.736 0.030 178 180 D Soyuz-TM 34 * 3M [Soyuz] R 2002 20 A [27416] BAI-LC1 2002 Apr 25.268 198.735 days 2002 Nov 10.003 Cyl+ 2 panels+ 7.5 long 2002 Apr 25.51 beehive+sphere 2.3 to 2002 Apr 26.57 7250 2.72 maxdia 2002 Apr 27.15 2002 Apr 27.50 2002 Jun 11.81 2002 Jun 12.71 2002 Jun 14.88 2002 Jul 31.45 2002 Aug 1.77 2002 Oct 17.83 2002 Oct 18.80 2002 Nov 6.86 2002 Nov 9.75 51.62 51.63 51.63 51.63 51.64 51.63 51.64 51.64 51.64 51.64 51.63 51.64 51.64 89.62 89.62 89.60 92.40 92.28 92.53 92.43 92.32 92.48 92.35 92.48 92.40 92.38 6634 6634 6633 6771 6765 6766 6773 6767 6774 6769 6775 6771 6770 242 244 243 387 382 384 389 382 384 377 386 383 382 269 267 265 398 390 391 399 394 408 403 406 402 401 0.002 0.002 0.002 0.0008 0.0006 0.0006 0.0007 0.0009 0.002 0.002 0.001 0.001 0.001 113 109 110 9 187 198 236 58 91 15 44 110 120 D Soyuz 3rd stage (Block I) 2002 20 B [27417] 2002 Apr 25.57 1.2 days 2002 Apr 26.7 Cylinder 2400? 8.1 long 2.66 dia 2002 Apr 25.63 2002 Apr 26.73 51.62 51.65 88.40 6574 86.63 6486 185 69 206 146 0.002 0.006 87 147 Spot 5 [Ariane-42P] (V151 #112) 2002 21 A [27421] KOU-ELA2 2002 May 4.06 Box + panel 3030 3.1x3.1 x5.7 2002 2002 2002 2012 May May May Jan 4.49 8.91 15.88 11.22 98.75 97.75 98.75 98.67 100.97 101.23 101.40 101.40 7183 7196 7203 7203 803 816 824 824 805 818 825 825 0.0001 0.0001 0.00008 0.00009 134 100 103 114 Idefix + # Ariane-4 3rd stage (H-10-3)+VEB 2002 21 B [27422] 2002 May 4.06 Cylinder 1670 + 520 cylinder 10.02 long 2.6 dia 1.03x4.0 2002 2002 2002 2012 May May May Jan 4.14 4.21 4.84 11.21 98.73 98.73 98.72 98.42 100.90 100.82 100.85 100.78 7180 7175 7177 7174 797 792 793 787 805 802 805 805 0.0004 0.0007 0.0009 0.001 218 193 286 349 D * # Apr Apr Apr Apr Apr May May May May May Jun Jan Page 2002 -9 Nodal period (min) Crew of 2 cosmonauts (Gidzenko, Vittori)and a space tourist (Shuttleworth) docked with ISS (Zarya nadir port) 2003 Apr 27.330; Finally undocked 2002 Nov 9.864 with Soyuz-TMA1 crew (Zalyotin, De Winne, Lonchakov). French amateur radio payload. 2014-version 1.13 Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Size (m) Lifetime Date of orbital determination Orbital Inclination (deg) Box + panel 3117 6.49 long x2.68x2.49 16.40 span 2002 2002 2002 2002 2002 2002 2012 98.18 98.17 98.17 98.18 98.17 98.17 98.22 98.30 98.35 98.45 98.53 98.65 98.82 98.82 Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) 7056 7058 7063 7067 7073 7081 7081 673 673 676 681 388 699 701 682 686 693 696 700 705 703 0.0006 0.0009 0.001 0.001 0.0009 0.0005 0.0001 176 149 67 70 119 111 85 2002 22 A [27424] VDB 2002 May 4.41 Delta-2 2nd stage 2002 22 B [27425] 2002 May 4.41 59 days 2002 Jul 2 2002 May 4.52 2002 Jul 2.30 97.41 97.32 93.55 87.17 6826 6513 217 120 678 148 0.034 0.002 259 47 DirecTV 5 (Tempo 1) 2002 23 A [Proton-K] [27426] BAI 2002 May 7.71 > million years 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2012 51.71 17.66 6.41 0.22 0.13 0.08 0.07 0.06 0.06 0.07 0.08 0.04 0.01 630.92 759.00 991.83 1406.83 1430.05 1434.47 1434.22 1436.05 1428.90 1434.58 1435.77 1436.08 1436.08 24368 27563 32945 41590 42046 42133 42128 42164 42024 42135 42158 42165 42164 194 6568 17333 34643 35591 35656 35646 35777 35521 35739 35752 35773 35773 35784 35800 35799 35779 35745 35853 35852 35793 35769 35775 35808 35799 35798 0.730 0.530 0.280 0.014 0.002 0.002 0.002 0.0002 0.003 0.0004 0.0007 0.0003 0.0003 0 359 359 11 250 138 129 172 68 112 199 244 247 D Proton-K 3rd stage [8S812) 2002 23 B [27427] 2002 May 7.71 2 days 2002 May 9 Cylinder 4185 4 long 4.1 dia 2002 May 7.70 2002 May 8.98 51.60 51.60 88.23 6566 87.40 6525 154 126 221 166 0.005 0.003 273 228 D Proton-K 4th stage Casing 2002 23 C [27428] 2002 May 7.71 1 day 2002 May 8 Hollow cyl 800? 4.0 long 3.7 dia 2002 My 7.95 2002 May 8.21 51.59 51.59 88.18 6563 87.28 6518 162 131 208 148 0.004 0.001 225 270 Proton-K 4th stage (Block DM) 2002 23 D [27429] 2002 May 7.71 > million years Cylinder 2350? 6.22 long 3.7 dia 2002 May 8.25 2012 Jan 9.65 17.66 18.04 755.52 27478 755.57 27480 6431 6430 35769 35772 0.534 0.534 359 32 Hai Yang 1 [CZ-4B] 2002 24 A [27430] TY 2002 May 15.08 2002 2002 2002 2002 2002 2012 98.57 98.76 98.80 98.80 98.79 98.35 270 839 815 799 792 785 284 882 819 816 794 798 0.001 0.003 0.0003 0.001 0.0002 0.0009 141 157 109 189 96 186 May May May May May May May May Jun Jun Jun Jun Jan May May May May May Jan 4.45 13.81 5.84 9.27 10.70 18.80 11.02 Page 2002 -10 Semi major axis (km) Aqua * (EOS-PM1) [Delta-2] D May May Jun Jun Jun Jun Jan Nodal period (min) 7.76 8.10 9.64 11.93 13.73 14.34 15.48 19.84 5.43 7.65 9.30 20.42 11.08 15.08 15.19 23.50 23.90 29.15 10.73 90.05 102.15 101.23 101.03 100.73 100.70 6656 7239 7195 7186 7172 7170 2002 24 continued on next page * Earth Observation Satellite that crosses the equator at 14:30 local time to the north; monitors the Earth’s water cycle. 2014-version 1.13 Year of Launch 2002 Name [Launcher] Fragment D D Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Date of orbital determination Orbital Inclination (deg) Size (m) Lifetime Nodal period (min) Page 2002 -11 Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) Feng Yun-1 4 2002 24 B [27431] 2002 May 15.08 2002 May 15.27 2002 May 15.55 2012 Jun 10.94 98.81 98.81 98.74 102.17 102.18 102.17 7240 7240 7240 852 852 850 870 872 872 0.001 0.001 0.001 194 191 279 CZ-4B 3rd stage 2002 24 C [27432] 2002 May 15.08 2002 May 15.27 2012 Jan 10.45 98.71 98.70 101.88 101.85 7226 7225 811 810 884 882 0.005 0.005 278 270 Fragments 2002 24 D-K Ofeq 5 [Shavit] 2002 25 A [27434] PMC 2002 May 28.64 No TLE available Shavit stage 2002 25 B [27435] 2002 May 28.64 95 days 2002 Aug 31 2002 May 28.77 2002 Aug 31.50 143.77 143.45 94.98 87.42 6897 6525 262 135 774 158 0.037 0.002 74 205 Cosmos 2389 [Kosmos-3M] 2002 26 A [27436] PLE 2002 May 28.76 2002 May 28.82 2002 May 30.20 2012 Jan 11.20 82.95 82.95 82.95 104.77 104.75 104.73 7362 7361 7361 950 949 948 1016 1016 1015 0.004 0.005 0.005 287 282 204 Kosmos-3M 2nd stage 2002 26 B [27437] 2002 May 28.76 2002 May 28.82 2002 May 28.89 2012 Jan 9.75 82.95 82.95 82.95 104.57 104.63 104.62 7353 7356 7255 946 949 943 1003 1005 1009 0.004 0.004 0.004 290 289 173 Intelsat 905 [Ariane-44L] (V152 #113) 2002 27 A [27438] KOU-ELA2 2002 Jun 6.28 > million years Box+ 2 panels 4723 1984 2.80x2.80 x5.90 31 span 2002 2002 2002 2002 2002 2002 2002 2002 2012 5.52 8.20 12.50 12.51 16.21 16.73 18.18 20.26 13.05 7.05 2.57 0.54 0.28 0.12 0.10 0.10 0.11 0.02 633.07 839.70 1194.03 1327.10 1432.87 1435.17 1436.07 1436.10 1436.08 24423 29483 37283 40003 42102 42147 42164 42165 42165 191 10379 25994 31459 35644 35741 35770 35775 35776 35898 35830 35814 35791 35802 35795 35801 35797 35796 0.731 0.432 0.132 0.054 0.002 0.0006 0.0004 0.0003 0.0002 178 178 172 163 140 159 146 200 218 Ariane-4 3rd stage (H-10-3)+VEB 2002 27 B [27439] 2002 Jun 6.28 513 days 2003 Nov 1 Cylinder 1670 + 520 Cylinder 11.05 long 2.6 dia 1.03x4.0 2002 Jun 5.52 2003 Oct 30.82 6.80 7.04 658.68 91.00 25078 6702 211 117 37186 530 0.737 0.031 177 221 2014-version 1.13 7 pieces, all in orbit For orbital information see extra pages at end of year Jun Jun Jun Jun Jun Jun Jun Jun Jan Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] D STS-111 # 7M Endeavour R [Shuttle] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Size (m) Lifetime Date of orbital determination Orbital Inclination (deg) Delta wing 116523 ↑ 99385 ↓ 37.5 long 5.5 dia 23.8 span 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 Jun Jun Jun Jun Jun Jun Jun Jun Jun Jun Jun Jun Jun 5.92 6.04 6.98 7.52 7.68 10.92 11.00 12.64 12.70 14.25 14.92 15.75 19.25 51.63 51.63 51.63 51.64 51.64 51.64 51.64 51.64 51.63 51.63 51.64 51.63 51.63 88.38 90.17 90.75 92.13 92.27 92.25 92.28 92.28 92.32 92.30 92.43 91.90 91.90 2002 2002 2002 2002 2002 2002 2002 2012 Jun Jun Jun Jun Jul Jul Jul Jan 10.11 10.43 27.72 29.81 3.86 5.72 15.71 12.98 48.63 0.20 0.17 0.17 0.17 0.16 0.14 2.20 638.35 1453.17 1438.43 1435.97 1434.85 1436.17 1436.12 1436.08 Nodal period (min) Page 2002 -12 Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) 6573 6662 6690 6758 6764 6763 6765 6765 6766 6766 6773 6746 6746 155 232 233 369 381 381 382 382 383 384 389 344 347 235 334 390 389 389 389 390 390 392 391 399 391 387 0.006 0.008 0.012 0.002 0.0006 0.0006 0.0006 0.0006 0.0007 0.0005 0.0007 0.003 0.003 343 183 184 174 165 169 181 167 194 199 235 356 19 24558 42498 42211 42162 42140 42166 42165 42165 238 36091 35797 35735 35734 35780 35780 35778 36121 36148 35867 35832 35790 35795 35793 35794 0.731 0.0007 0.0008 0.001 0.0007 0.0002 0.0002 0.0002 0 295 263 230 219 257 251 259 2002 28 A [27440] CC-LC39A 2002 Jun 5.891 13.858 days 2002 Jun 19.749 Express-A 4 [Proton-K] 2002 29 A [27441] BAI 2002 Jun 10.05 > million years D Proton-K 3rd stage [8S812) 2002 29 B [27442] 2002 Jun 10.05 2.3 days 2002 Jun 12.4 Cylinder 4185 4 long 4.1 dia 2002 Jun 10.04 2002 Jun 12.36 51.64 51.63 88.28 6568 86.92 6500 187 118 192 125 0.0004 0.0006 278 259 D Proton-K 4th stage Casing 2002 29 C [27443] 2002 Jun 10.05 0.5 day 2002 Jun 11.0 Hollow cyl 800? 4.0 long 3.7 dia 2002 Jun 10.35 2002 Jun 10.78 51.62 51.62 88.23 6566 87.68 6539 183 157 191 163 0.0006 0.0004 69 45 Proton-K 4th stage (Block DM) 2002 29 D [27444] 2002 Jun 10.05 > million years Cylinder 2350? 6.22 long 3.7 dia 2002 Jun 11.85 2012 Jan 12.76 0.24 8.48 1450.72 42451 1450.60 42448 36006 36018 36138 36121 0.002 0.001 332 251 D Proton-K Ullage motor 2002 29 E [27447] 2002 Jun 10.05 440 days 2003 Aug 24 Cylinder 56 2002 Jun 17.66 2003 Aug 24.45 47.39 46.30 640.32 24609 89.73 6640 329 102 36132 420 0.727 0.024 2 25 D Proton-K Ullage motor 2002 29 F [27448] 2002 Jun 10.05 196 days 2002 Dec 23 Cylinder 56 2002 Jun 16.32 2002 Dec 23.13 47.41 46.63 639.18 24580 108.62 7542 270 92 36133 2234 0.730 0.142 2 70 # Crew of 7 astronauts (Cockrell, Lockhart, Chang-Diaz, Perrin, Korzun, Treschyov and Whitson) docked with ISS (PMA-2/Destiny port) 2002 Jun 8.684; undocked 2002 Jun 15.605. Korzun, Treschyov and Whitson stayed on board ISS; Onufrienko, Walz and Bursch returned with the shuttle at Edwards AFB After a two day delay due to bad weather at Kennedy Space Center. 2014-version 1.13 Year of Launch 2002 Name [Launcher] Fragment D Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Date of orbital determination Orbital Inclination (deg) 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2012 16.00 19.64 22.66 24.45 26.41 26.75 27.51 5.70 9.40 9.80 15.87 16.95 18.16 18.62 28.75 29.84 1.30 1.88 2.59 3.27 5.90 6.40 12.26 4.30 12.40 13.38 13.13 0.02 0.75 0.11 0.20 0.20 0.19 0.21 0.20 0.19 0.09 0.18 0.16 0.12 0.13 0.15 0.11 0.13 0.12 0.14 0.10 0.11 0.12 0.10 0.05 0.01 0.02 0.02 Size (m) Lifetime Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) 746.67 884.83 1287.97 1408.72 1436.03 1422.00 1436.03 1432.58 1430.73 1436.60 1440.10 1429.88 1437.55 1434.23 1435.95 1438.92 1434.85 1438.73 1437.37 1432.53 1441.78 1439.27 1436.10 1445.25 1435.97 1436.10 1436.10 27263 30531 39213 41627 42163 41888 42164 42096 42060 42175 42243 42043 42193 42128 42162 42220 42141 42216 42190 42095 42276 42227 42165 42344 42162 42165 42165 382 6868 24265 29080 30151 29596 30151 30251 30829 31025 32152 32132 32424 32446 33929 34338 34685 34862 34986 34797 35582 35581 35783 35902 35781 35784 35785 41388 41437 41404 41417 41418 41423 41419 41184 40533 40567 39577 39198 39205 39053 37638 37345 36839 36813 36636 36636 36213 36116 35790 36028 35786 35788 35788 0.752 0.566 0.219 0.148 0.134 0.141 0.134 0.130 0.115 0.113 0.088 0.084 0.080 0.078 0.044 0.036 0.026 0.023 0.020 0.022 0.007 0.006 0.00008 0.001 0.00006 0.00005 0.00004 64 182 328 344 347 345 346 343 341 28 296 342 357 346 341 344 345 350 349 339 353 354 209 230 240 200 351 Galaxy 3C [Zenit-3 SL] 2002 30 A [27445] ODS 2002 Jun 15.94 > million years Zenit-3 SL 3rd Stage (Block DM-SL) 2002 30 B [27446] 2002 Jun 15.94 Cylinder 2140 6.22 long 3.7 maxdia 2002 Jun 16.00 2002 Jun 16.52 2012 Jan 12.62 0.14 0.01 0.79 747.48 27284 745.15 27226 741.70 27143 385 339 410 41425 41356 41117 0.752 0.753 0.750 44 93 284 Iridium 97 2002 31 A [Rokot / Breeze-KM] [27450] PLE 2002 Jun 20.40 Box+ 2 panels 657 full 556 empty 1 across 3.5 long 2002 2002 2002 2007 2012 Jun Jun Jul Jan Jan 20.39 20.59 10.14 9.06 13.51 86.59 86.59 86.58 86.40 86.39 92.75 98.02 98.17 100.40 100.40 6788 7042 7049 7156 7156 157 658 666 773 776 661 669 676 781 779 0.037 0.0007 0.0007 0.0005 0.0002 151 76 11 88 175 Iridium 98 2002 31 B [27451] 2002 Jun 20.40 Box+ 2 panels 657 full 556 empty 1 across 3.5 long 2002 2002 2005 2002 2012 Jun Jul Jul Jun Jan 20.45 10.13 15.33 17.53 13.36 86.58 86.58 86.82 87.23 86.45 97.97 98.17 98.75 99.78 99.78 7040 7049 7078 7126 7127 657 667 696 744 746 666 674 702 752 750 0.0007 0.0005 0.0004 0.0006 0.0003 42 343 102 121 190 Breeze-KM 3rd stage 2002 31 C [27452] 2002 Jun 20.40 149 days 2002 Nov 16 2002 Jun 20.52 2002 Nov 16.54 86.58 86.52 6825 6504 231 112 662 139 0.032 0.002 316 126 2014-version 1.13 Jun Jun Jun Jun Jun Jun Jun Jul Jul Jul Jul Jul Jul Jul Jul Jul Aug Aug Aug Aug Aug Aug Aug Sep Sep Sep Jan Page 2002 -13 Nodal period (min) 93.52 87.00 Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Date of orbital determination Orbital Inclination (deg) Size (m) Lifetime Nodal period (min) Page 2002 -14 Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) NOAA 17 # [Titan 23G] 2002 32 A [27453] VDB 2002 Jun 24.77 2002 Jun 24.84 2002 Jun 25.11 2012 Jan 13.43 98.79 98.79 98.35 101.20 101.18 101.08 7194 7193 7189 808 806 802 823 823 818 0.001 0.001 0.001 333 332 252 Fragment? 2002 32 B [38555] 2012 Jul 2.55 98.77 96.78 6983 592 617 0.002 120 D Progress-M 46 * [Soyuz-U] 2002 33 A [27454] BAI-LC1 2002 Jun 26.234 110.198 days 2002 Oct 14.432 Cyl+ 2 panels+ 7.9 long 2002 Jun 26.29 beehive+sphere 2.12 maxdia 2002 Jun 26.67 7265 2002 Jun 28.82 2002 Jul 31.45 2002 Aug 1.77 2002 Sep 24.83 2002 Sep 25.02 2002 Sep 25.08 2002 Sep 30.77 2002 Oct 14.29 51.61 51.63 51.63 51.64 51.64 51.63 51.64 51.66 51.63 51.63 88.53 89.95 92.42 92.32 92.48 92.32 91.73 91.98 92.27 92.15 6581 6651 6772 6767 6774 6765 6738 6750 6764 6759 187 267 388 382 384 375 333 340 357 363 217 277 398 394 408 399 386 404 414 397 0.002 0.0007 0.0008 0.0009 0.002 0.002 0.004 0.005 0.004 0.003 85 171 293 58 91 300 216 197 304 6 D Soyuz-U 3rd stage (Block I) 2002 33 B [27455] 2002 Jun 26.23 1.9 days 2002 Jun 28.1 Cylinder 2400? 2002 Jun 26.54 2002 Jun 27.88 51.66 51.61 89.28 6618 87.57 6532 202 150 277 157 0.006 0.0006 208 108 Contour % [Delta-2 7425] 2002 34 A [27457] CC 2002 Jul 3.28 Octagonal cyl 775 2002 Jul 3.33 2002 Aug 6.71 30.50 30.55 2431.05 2486.892 59890 60791 91 212 106933 0.892 108614 0.892 336 340 D Delta-2 2nd stage 2002 34 B [27458] 2002 Jul 3.28 4 days 2002 Jul 7 2002 Jul 3.33 2002 Jul 7.19 30.42 30.67 89.23 86.92 6615 6501 174 122 300 122 0.009 0 336 358 D Delta-2 3rd stage (PAM-D) 2002 34 C [27459] 2002 Jul 3.28 469 days 2003 Oct 15 2002 2003 2003 2003 30.49 31.64 31.52 31.32 2418.42 2254.98 890.83 106.92 59683 59963 30669 7463 90 111 98 82 106518 101057 48482 2086 0.892 0.886 0.789 0.134 336 34 34 40 # * % American weather satellite. Titan 23G stage de-orbited on first orbit. Progress-M 46 docked 2002 Jun 29.266 with ISS (Zvevda aft port); undocked 2002 Sep 24.583. Stayed 3 weeks in orbit before de-orbiting. Comet Nucleus TOUR was to fly-by two comet nuclei and possible a 3rd. After ignition on 2002 Aug 15.367 of the solid rocket motor intended to inject the spacecraft into solar orbit, contact with the probe could not be re-established. Ground-based telescopes later found three objects along the course of the satellite, leading to the speculation that it had been destroyed. Attempts to contact the probe were ended on 20 December 2002. 2014-version 1.13 8.1 long 2.66 dia Jul Oct Oct Oct 3.33 10.85 11.15 15.27 Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Size (m) Lifetime Date of orbital determination Orbital Inclination (deg) Page 2002 -15 Nodal period (min) Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) Atlantic Bird 3 (Stellat 5) [Ariane-5] (V153 #512) 2002 35 A [27460] KOU-ELA3 2002 Jul 5.97 > million years Box+2 panels 4050 1805 dry 2.44x3.45 x5.37 37 span 2002 2002 2002 2002 2002 2002 2002 2012 Jul Jul Jul Jul Jul Jul Jul Jan 6.21 7.03 7.66 9.90 17.61 24.59 29.10 14.18 5.47 5.02 1.17 0.12 0.12 0.09 0.09 0.05 636.65 675.92 959.88 1320.90 1431.45 1436.17 1436.10 1436.08 24515 25513 32233 39879 42074 42166 42165 42165 589 2182 15951 31337 35684 35787 35784 35765 35683 36086 35759 35663 35707 35788 35788 35807 0.716 0.664 0.307 0.054 0.0003 0.00002 0.00004 0.0005 178 180 179 228 333 200 89 271 N Star C 2002 35 B [27461] 2002 Jul 5.97 > million years Box+ 2 panels 1645 + 5m dish 1.5x1.9 x3.3 12.6 span 2002 2002 2002 2002 2002 2002 2002 2002 2012 Jul Jul Jul Jul Jul Jul Jul Aug Jan 5.77 8.28 9.08 10.82 12.71 13.44 29.03 19.54 13.54 5.49 3.06 1.90 0.19 0.06 0.06 0.05 0.03 0.60 636.82 739.65 949.62 1312.70 1434.17 1447.82 1435.78 1436.10 1436.13 24519 27092 32003 39713 42127 42394 42159 42165 42166 583 5699 15486 30888 35446 35853 35771 35774 35778 35698 35728 35764 35781 36051 36178 35789 35799 35796 0.716 0.554 0.317 0.062 0.007 0.004 0.0002 0.0003 0.0002 178 179 180 175 59 166 88 323 212 Ariane-5 2nd stage (EPS)+VEB 2002 35 C [27462] 2002 Jul 5.97 Drum-cone 1190+1500 Cylinder 3.36 long 3.94 dia 1.56x4.56 2002 2002 2002 2002 2012 Jul Jul Jul Jul Jan 5.79 6.66 7.60 8.90 13.96 5.44 5.48 5.47 5.48 5.33 638.13 647.18 646.95 647.02 646.77 24553 24785 24779 24780 24774 605 625 622 623 626 35744 36187 36178 36180 36165 0.716 0.717 0.717 0.717 0.717 178 179 180 181 183 Sylda upperpart 2002 35 D [27463] 2002 Jul 5.97 Hollow cone 900 4.90 long 4.56 dia 2002 2002 2002 2002 2012 Jul Jul Jul Jul Jan 6.65 6.66 7.10 10.00 13.55 5.51 6.51 5.48 5.49 5.06 636.62 611.77 647.57 637.25 636.53 24514 23872 24795 24530 24512 529 473 625 598 593 35742 34513 36206 35705 35674 0.718 0.713 0.718 0.716 0.716 178 170 179 181 251 Cosmos 2390 [Kosmos-3M] 2002 36 A [27464] PLE 2002 Jul 8.28 2002 2002 2002 2012 Jul Jul Jul Jan 8.27 8.38 8.90 14.36 82.46 82.49 82.48 82.48 100.15 115.68 115.70 115.70 7144 7865 7866 7866 140 1467 1467 1468 1391 1506 1507 1506 0.088 0.003 0.003 0.002 63 309 302 258 Cosmos 2391 2002 36 B [27465] 2002 Jul 8.28 2002 2002 2002 2012 Jul Jul Jul Jan 8.42 8.90 10.19 14.35 82.48 82.49 82.48 82.48 115.70 115.73 115.67 115.67 7866 7867 7865 7864 1467 1468 1466 1466 1507 1509 1506 1505 0.003 0.003 0.003 0.002 305 296 305 259 Kosmos-3M 2nd stage 2002 36 C [27466] 2002 Jul 8.28 2002 Jul 8.42 2002 Jul 8.45 2012 Jan 14.21 82.49 82.49 82.48 115.72 115.73 115.72 7866 7867 7867 1468 1468 1455 1508 1508 1521 0.003 0.003 0.004 298 299 271 Fragments 2002 36 D 2002 36 E [27533] [27546] 2002 Sep 25.69 2002 Oct 23.64 82.49 82.49 115.70 115.67 7866 7864 1466 1463 1508 1508 0.003 0.003 128 69 2014-version 1.13 Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Date of orbital determination Orbital Inclination (deg) 2002 2002 2002 2003 2003 2012 25.79 7.71 10.61 17.90 10.09 13.84 63.47 63.48 63.48 63.45 63.44 63.44 Size (m) Lifetime Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) 8054 8027 8015 8030 8029 8029 1512 1511 1511 1499 1496 1369 1840 1785 1762 1803 1804 1931 0.020 0.017 0.016 0.019 0.019 0.035 0 359 359 358 357 351 2002 37 A [27470] BAI 2002 Jul 25.63 > million years D Proton-K 3rd stage [8S812) 2002 37 B [27471] 2002 Jul 25.63 0.7 days 2002 Jul 26.3 Cylinder 4185 4 long 4.1 dia 2002 Jul 25.87 2002 Jul 26.12 64.86 64.86 87.52 6530 87.25 6517 145 132 158 145 0.001 0.001 226 257 D Proton-K 4th stage Casing 2002 37 C [27472] 2002 Jul 25.63 0.4 day 2002 Jul 26.0 Hollow cyl 800? 4.0 long 3.7 dia 2002 Jul 25.87 2002 Jul 26.05 64.86 64.86 87.37 6523 87.30 6519 136 104 152 177 0.001 0.006 144 155 Proton-K 4th stage (Block DM5) 2002 37 D [27473] 2002 Jul 25.63 > million years Cylinder 2350? 6.22 long 3.7 dia 2002 Jul 25.87 2012 Jan 13.93 63.47 63.45 119.85 8053 119.85 8053 1509 1371 1839 1977 0.020 0.038 0 348 D Proton-K Ullage motor 2002 37 E [27474] 2002 Jul 25.63 1314 days 2006 Feb 28 Cylinder 56 2002 Jul 26.02 2006 Feb 28.55 63.79 63.70 116.95 7922 87.15 6512 199 124 2888 142 0.170 0.001 211 56 D Proton-K Ullage motor 2002 37 F [27475] 2002 Jul 25.63 1009 days 2005 Apr 29 Cylinder 56 2002 Jul 26.43 2005 Apr 29.27 63.79 63.60 116.88 7919 87.37 6522 193 137 2889 150 0.170 0.001 211 174 Fragments 2002 37 G-BV Hot Bird 6 [Atlas 5] 2002 38 A [27499] CC 2002 Aug 21.92 > million years 2002 2002 2002 2002 2002 2002 2002 2002 2002 2012 21.65 24.66 27.32 31.60 31.94 5.22 15.80 24.93 29.84 17.85 17.53 10.63 1.23 0.09 0.09 0.09 0.07 0.07 0.06 0.09 827.83 946.85 1589.33 1436.38 1435.48 1436.05 1432.18 1433.32 1436.05 1436.08 29205 31941 45113 42173 42153 42164 42088 42111 42164 42165 304 5503 31815 35720 35689 35781 35695 35695 35767 35762 45349 45622 45655 35869 35860 35790 35724 35769 35803 35810 0.771 0.628 0.153 0.002 0.002 0.0001 0.0003 0.0009 0.0004 0.0006 179 181 182 42 63 12 152 261 263 20 Atlas-5 2nd stage (Centaur) 2002 38 B [27500] 2002 Aug 21.92 2002 Aug 21.65 2012 Jan 19.26 18.05 18.30 790.52 590.47 28321 23315 286 213 43599 33659 0.765 0.717 181 318 2014-version 1.13 119.88 119.28 119.02 119.33 119.32 119.32 Page 2002 -16 Semi major axis (km) Cosmos 2392 [Proton-K] 60 pieces, 51 have decayed Jul Aug Aug Jul Aug Jan Nodal period (min) For orbital information see extra pages at end of year Aug Aug Aug Aug Aug Sep Sep Sep Sep Jan Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Date of orbital determination Orbital Inclination (deg) 2002 2002 2002 2002 2002 2002 2002 2002 2012 Aug Aug Aug Aug Aug Sep Sep Oct Jan 22.25 22.74 24.87 26.11 27.48 10.39 30.68 21.09 20.10 Size (m) Lifetime Page 2002 -17 Nodal period (min) Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) 22.99 23.01 10.97 6.43 0.23 0.06 0.04 0.02 0.03 717.30 712.82 858.93 985.10 1403.40 1436.10 1424.10 1436.08 1436.12 26544 26433 29932 32796 41523 42165 41930 42165 42165 4489 4269 11267 16998 34470 35777 35541 35775 35773 35841 35840 35840 35836 35818 35795 35561 35797 35800 0.591 0.597 0.410 0.287 0.016 0.0002 0.0002 0.0003 0.0003 359 359 359 0 20 242 221 87 252 Echostar-8 [Proton-K] 2002 39 A [27501] BAI 2002 Aug 22.22 > million years Proton-K 4th stage (Block DM3) 2002 39 B [27504] 2002 Aug 22.22 Cylinder 2350? 6.22 long 3.7 dia 2002 2002 2002 2012 Aug Aug Aug Jan 22.25 22.75 23.73 18.82 51.68 24.70 23.25 22.49 630.43 712.45 713.42 713.45 24355 26424 26448 26449 144 4273 4276 4212 35809 35818 35862 35928 0.732 0.597 0.597 0.600 0 358 359 214 Atlantic Bird 1 [Ariane-5] (V155 #513) 2002 40 A [27508] KOU-ELA3 2002 Aug 28.95 > million years Box+ 2 panels 2700 1550 dry 2.0x2.1 x2.8 19 span 2002 2002 2002 2002 2002 2002 2012 Aug Sep Sep Sep Sep Sep Jan 28.75 5.47 7.86 8.67 9.73 16.82 19.96 5.43 0.04 0.04 0.04 0.05 0.04 0.0005 641.13 1417.00 1425.87 1436.03 1436.80 1436.10 1436.08 24630 41790 41965 42164 42179 42165 42165 585 34954 34294 35724 35790 35780 35765 35917 35869 35878 35846 35810 35793 35807 0.717 0.011 0.007 0.001 0.0002 0.0002 0.0005 178 187 178 162 84 284 344 Meteosat Second Generation 1 2002 40 B [27509] 2002 Aug 28.95 > million years Cylinder 2000 1000 dry 2.4 high 3.2 dia 2002 2002 2002 2002 2002 2002 2008 2008 2008 2008 2008 2008 2012 Aug Sep Sep Sep Sep Sep Apr Apr Apr Apr May May Jan 28.75 3.65 3.71 7.99 9.70 18.83 2.11 4.80 6.94 30.90 7.86 25.75 18.99 5.40 0.92 0.95 2.05 2.08 1.98 0.46 0.46 0.46 0.47 0.50 0.52 1.05 639.90 1093.23 1089.77 1431.62 1423.35 1436.08 1436.02 1434.42 1434.08 1436.22 1436.18 1436.08 1436.03 24598 35154 35079 42077 41915 42164 42164 42132 42125 42167 42167 42165 42164 586 21679 21671 35540 35531 35749 35780 35751 35742 35778 35781 35761 35778 35853 35872 35731 35857 35542 35823 35791 35756 35751 35799 35795 35811 35792 0.717 0.202 0.200 0.004 0.0001 0.0009 0.0001 0.00005 0.0001 0.0002 0.0002 0.0006 0.0002 177 15 13 34 349 159 329 40 266 43 6 62 140 Ariane-5 2nd stage (EPS)+VEB 2002 40 C [27510] 2002 Aug 28.95 Drum-cone 1190+1500 Cylinder 3.36 long 3.94 dia 1.56x4.56 2002 Aug 28.76 2012 Jan 19.73 5.46 5.09 634.23 633.97 24453 24446 569 571 35580 35563 0.716 0.716 177 263 Sylda upperpart 2002 40 D [27511] 2002 Aug 28.95 Hollow cone 900 4.90 long 4.56 dia 2002 Aug 28.75 2002 Aug 29.64 2012 Jan 15.77 5.51 5.46 5.73 637.03 641.20 640.20 24525 24631 24606 564 589 583 35728 35917 35873 0.717 0.717 0.717 178 178 203 MSG 1 Cooler cover MSG 1 Baffle Cover 2002 40 E 2002 40 F [39998] [39999] 2014 Mar 18.69 2014 Jun 5.77 7.83 7.87 1423.40 1412.13 41916 41695 35448 34927 35627 35705 0.002 0.009 128 16 2014-version 1.13 Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Size (m) Lifetime Date of orbital determination Orbital Inclination (deg) Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) Intelsat 906 [Ariane-44L] (V154 #114) 2002 41 A [27513] KOU-ELA2 2002 Sep 6.28 > million years Box+ 2 panels 4723 2.80x3.50 x5.56 31 span 2002 2002 2002 2002 2002 2002 2002 2012 6.08 7.44 9.51 11.75 12.60 16.67 18.47 19.95 7.00 3.46 0.51 0.18 0.42 0.09 0.09 0.01 658.73 756.58 1154.85 1360.75 1235.98 1435.35 1436.08 1436.08 25079 27504 36882 40677 38154 42150 42165 42164 155 6437 25221 32829 27762 35758 35779 35774 37245 35815 35786 35767 35782 35785 35793 35798 0.739 0.534 0.143 0.036 0.105 0.0003 0.0002 0.0003 177 178 178 179 183 288 200 312 D Ariane-4 3rd stage (H-10-3)+VEB 2002 41 B [27514] 2002 Sep 6.28 89 days 2002 Dec 4 Cylinder 1670 + 520 Cylinder 11.05 long 2.6 dia 1.03x4.0 2002 Sep 6.08 2002 Sep 26.13 2002 Dec 4.00 7.05 6.98 6.74 631.15 536.97 103.55 24374 21884 7305 169 92 176 35821 30918 1677 0.731 0.704 0.103 178 196 43 D Users SEM * [H-2A #3] 2002 42 A [27515] TAN-YLP1 2002 Sep 10.35 1739 days 2007 Jun 15 800 2002 2002 2002 2003 2003 2005 2005 2007 Sep Sep Sep May Jun Feb Feb Jun 10.40 16.95 17.70 29.80 13.30 2.01 28.47 14.28 30.29 30.41 30.41 30.41 30.40 30.41 30.44 30.34 93.55 93.47 94.83 94.18 96.18 95.98 93.77 88.35 6827 6823 6889 6857 6954 6945 6837 6572 440 437 503 473 570 562 455 185 456 451 518 484 582 571 462 200 0.001 0.001 0.001 0.0009 0.0009 0.0006 0.0005 0.001 271 328 355 115 283 211 133 340 Kodama (DRTS)& 2002 42 B [27516] 2002 Sep 10.35 > million years 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2012 Sep Sep Sep Sep Sep Oct Oct Oct Oct Oct Jan 10.46 10.59 11.58 12.69 17.49 7.60 10.45 10.60 11.63 15.66 20.15 30.40 28.40 11.95 0.34 0.10 0.07 0.03 0.05 0.06 0.05 1.08 93.58 641.13 780.98 1393.17 1446.87 1434.47 1438.55 1436.55 1436.05 1436.08 1436.08 6828 24630 28092 41320 42375 42133 42213 42174 42164 42165 42165 443 465 7414 33858 35944 35667 35786 35777 35768 35773 35777 456 36038 36013 36026 36049 35841 35882 35814 35803 35800 35795 0.001 0.722 0.509 0.026 0.001 0.002 0.001 0.0004 0.0004 0.0003 0.0002 270 179 179 162 39 319 333 263 290 285 237 H-2A 2nd stage 2002 42 D [27518] 2002 Sep 10.35 2002 Sep 15.68 2012 Jan 19.34 28.44 28.91 613.27 611.25 23911 23859 476 445 34589 34515 0.713 0.714 182 38 Users REM $ 2002 42 H [27815] 2002 Sep 10.35 261 days 2003 May 29 2003 2003 2003 2003 2003 30.41 30.40 30.40 30.40 30.40 94.23 94.52 95.35 96.20 96.18 6860 6874 6914 6955 6954 474 489 529 570 570 489 502 542 582 582 0.001 0.0009 0.0009 0.0009 0.0009 128 161 182 196 283 D 926 4 pieces, all have decayed 2.2 x 2.4 x 2.2 May Jun Jun Jun Jun 29.93 1.34 3.44 5.30 13.10 D Fragments * & Unmanned Space experiment Recovery System Service and Engeneering Module. $ Re-Entry Module Data Relay Test Satellite for inter-satellite communications. 2014-version 1.13 2002 42 C, E-G Box +2 panels 2800 1500 bol Sep Sep Sep Sep Sep Sep Sep Jan Page 2002 -18 Nodal period (min) For orbital information see extra pages at end of year Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Date of orbital determination Orbital Inclination (deg) 2002 2002 2002 2002 2012 Size (m) Lifetime Page 2002 -19 Nodal period (min) Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) 4.67 0.46 0.27 0.48 2.52 648.42 1399.68 1401.40 1436.08 1436.10 29687 41449 41483 42164 42165 12107 34508 34490 35771 35757 34510 35633 35719 35801 35816 0.377 0.014 0.15 0.0004 0.0007 180 36 152 334 206 2002 Sep 17.70 2012 Jan 19.80 17.75 17.74 606.73 157.28 23741 9652 197 139 34527 6408 0.723 0.325 183 191 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2012 sep Sep sep Sep Sep Oct Oct Nov Nov Nov Jan 18.65 19.24 20.38 25.89 27.07 1.14 6.25 1.80 8.88 20.64 20.02 20.85 20.90 10.96 0.75 0.12 0.10 0.10 0.07 0.05 0.03 0.04 846.38 832.38 959.50 1693.20 1431.78 1433.78 1436.08 1440.57 1435.95 1436.08 1436.12 29640 29312 32225 47058 42081 42119 42165 42252 42162 42165 42165 268 195 6059 35709 35681 35706 35784 35852 35763 35766 35762 46254 45672 45633 45649 35723 35776 35788 35895 35804 35806 35812 0.776 0.776 0.614 0.106 0.0005 0.0008 0.00004 0.0005 0.0005 0.0005 0.0006 179 179 180 176 5 301 280 338 320 300 358 2002 2003 2003 2003 Sep Mar Mar Apr 18.64 19.57 20.00 3.46 20.90 21.06 21.05 20.97 1436.82 754.15 551.60 95.28 29416 27445 22280 6911 231 168 125 208 45844 41965 31678 856 0.775 0.761 0.708 0.047 180 277 280 318 Kalpana 1 # (Metsat 1) [PSLV C4] 2002 43 A [27525] SRI 2002 Sep 12.43 Box + panel 1060 498 (dry) PSLV 4th stage 2002 43 B [27526] 2002 Sep 12.43 Cylinder 920 Hispasat 1D [Atlas 2AS] 2002 44 A [27528] CC-LC36A 2002 Sep 18.92 > million years D Centaur stage 2002 44 B [27529] 2002 Sep 18.92 197 days 2003 Apr 3 D Progress-M1 9 * [Soyuz-U] 2002 45 A [27531] BAI-LC1 2002 Sep 25.707 129.091 days 2003 Feb 1.798 Cyl+ 2 panels+ 7.9 long 2002 Sep 25.88 beehive+sphere 2.12 maxdia 2002 Sep 25.94 7265 2002 Sep 27.70 2002 Sep 27.97 2002 Sep 29.59 2002 Sep 29.77 2002 Oct 11.75 2002 Oct 12.77 2002 Oct 17.83 2002 Oct 18.80 2002 Nov 30.12 2002 Dec 1.84 2003 Jan 1.83 51.69 51.64 51.65 51.66 51.64 51.64 51.64 51.63 51.64 51.63 51.64 51.64 51.64 88.62 90.57 92.32 92.22 92.27 92.28 92.20 92.32 92.35 92.48 92.42 92.50 92.30 6584 6681 6767 6761 6764 6765 6761 6767 6769 6775 6771 6776 6766 125 280 375 371 375 374 371 377 377 386 387 394 383 287 325 401 394 396 398 394 399 403 406 398 399 391 0.012 0.003 0.002 0.002 0.002 0.002 0.002 0.002 0.002 0.001 0.0008 0.0004 0.0006 275 40 303 309 322 316 0 353 15 44 198 285 99 D Soyuz-U 3rd stage (Block I) 2002 45 B [27532] 2002 Sep 25.71 1.6 days 2002 Sep 27.3 Cylinder 2400? 51.62 51.65 88.43 6576 87.10 6509 185 128 210 133 0.002 0.0003 71 23 # * Renamed 2003 Feb 5 after Kalpana Chawla, US-Indian astronaut who died in the STS 107 Columbia accident 2003 Feb 1. Docked with ISS (Zvezda aft port) 2002 Sep 29.709; undocked 2003 Feb 1.667 2014-version 1.13 2.60 long 1.34 dia 2760 8.1 long 2.66 dia sep Sep Sep Sep Jan 13.67 17.00 22.20 25.83 16.77 2002 Sep 25.94 2002 Sep 27.23 Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Date of orbital determination Orbital Inclination (deg) Size (m) Lifetime Nodal period (min) Page 2002 -20 Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) Nadezhda-M [Kosmos-3M] 2002 46 A [27534] PLE 2002 Sep 26.60 2002 Sep 26.66 2002 Sep 29.50 2012 Jan 18.80 82.91 82.93 82.93 104.68 104.92 104.90 7358 7369 7369 943 965 964 1016 1016 1016 0.005 0.003 0.004 290 275 195 Kosmos-3M 2nd stage 2002 46 B [27535] 2002 Sep 26.60 2002 Sep 26.66 2012 Jan 19.77 82.93 82.93 104.77 104.78 7362 7363 962 957 1005 1011 0.003 0.004 278 163 D STS-112 # 7M Atlantis F26 R [Shuttle] 2002 47 A [27537] CC-LC39B 2002 Oct 7.823 10.833 days 2002 Oct 18.656 Delta wing 116538 ↑ 91390 ↓ 37.5 long 5.5 dia 23.8 span 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 7.85 8.00 8.85 9.54 9.75 12.25 12.57 14.61 17.62 17.85 18.25 51.63 51.64 51.63 51.64 51.63 51.63 51.63 51.63 51.64 51.64 51.64 88.38 89.00 89.12 92.18 92.22 92.20 92.32 92.38 92.33 91.32 91.30 6573 6604 6610 6760 6761 6761 6767 6770 6767 6717 6717 155 209 221 370 371 370 378 378 373 273 272 234 241 241 393 395 394 399 405 404 404 404 0.006 0.002 0.002 0.002 0.002 0.002 0.002 0.002 0.002 0.010 0.010 343 293 273 357 352 1 352 1 7 19 21 Integral [Proton-K] 2002 48 A [27540] BAI 2002 Oct 17.19 > million years Box +2 panels >4000 5 high 3.7 dia 16 soan 2002 Oct 17.25 2002 Oct 31.28 2012 Jan 20.25 51.74 52.22 70.93 3938.50 4313.23 4308.40 82613 87773 87708 848 9028 3062 151621 0.913 153762 0.824 159596 0.892 300 302 250 D Proton-K 3rd stage [8S812) 2002 48 B [27541] 2002 Oct 17.19 52 days 2002 Dec 8 Cylinder 4185 4 long 4.1 dia 2002 Oct 17.19 2002 Dec 8.80 51.64 51.54 93.00 6800 86.87 6498 187 106 656 133 0.034 0.002 80 284 D Proton-K 4th stage (Block DM2) 2002 48 C [27542] 2002 Oct 17.19 2939 days 2010 Nov 3 Cylinder 2350? 6.22 long 3.7 dia 2002 Oct 17.25 2010 Oct 30.71 51.79 85.17 3959.93 82912 3900.20 82076 841 280 152226 0.913 151116 0.919 300 243 D Proton-K 4th stage Casing 2002 48 D [27543] 2002 Oct 17.19 12 days 2002 Oct 29 Hollow cyl 800? 4.0 long 3.7 dia 2002 Oct 17.51 2002 Oct 29.21 51.55 51.53 93.42 6820 87.52 6530 205 129 678 174 84 124 Fragments 2002 48 E-H # 4 pieces, all have decayed Oct Oct Oct Oct Oct Oct Oct Oct Oct Oct Oct 0.035 0.003 For orbital information see extra pages at end of year Crew of 7 astronauts (Ashby, Melroy, Wolf, Sellers, Magnus, Yurchikhin) docked with ISS (PMA-2/Destiny port) 2002 Oct 9.636; undocked 2002 Oct 16.551. Installed the S1 truss. 2014-version 1.13 Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Date of orbital determination Orbital Inclination (deg) 2002 2003 2012 2015 27.25 22.70 20.92 22.51 97.27 97.38 97.07 97.09 94.32 94.43 94.00 87.23 2002 Oct 27.25 2007 Jan 5.96 97.40 97.11 94.13 87.17 D JB-3 B [CZ-4B] 2002 49 A [27550] TY-LC7 2002 Oct 27.14 4470 days 2015 Jan 22 Box +2 panels D CZ-4B 3rd stage 2002 49 B [27551] 2002 Oct 27.14 1532 days 2007 Jan 6 Cylinder 1730? D Fragments 2002 49 C-F Size (m) Lifetime 4.93 long 2.9 dia 4 pieces, all have decayed Oct Mar Jan Jan Nodal period (min) Page 2002 -21 Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) 6864 6870 6849 6516 397 484 464 134 574 499 476 140 0.013 0.001 0.0009 0.0005 282 49 55 228 6855 6513 470 129 483 139 0.0009 0.0007 285 280 For orbital information see extra pages at end of year D Soyuz-TMA 1 * 3M [Soyuz-FG] R 2002 50 A [27552] BAI-LC1 2002 Oct 30.133 185.953 days 2003 May 4.086 Cyl+ 2 panels+ 7.5 long 2002 Oct 30.19 beehive+sphere 2.3 to 2002 Oct 30.51 7220 2.72 maxdia 2002 Oct 31.31 2002 Nov 1.19 2002 Nov 26.51 2003 May 2.81 51.62 51.63 51.63 51.64 51.64 51.63 88.85 90.23 90.28 92.43 92.32 92.37 6596 6664 6667 6772 6766 6769 196 277 278 384 378 386 240 294 300 404 396 395 0.003 0.001 0.002 0.001 0.001 0.0006 86 87 56 92 177 78 D Soyuz 3rd stage (Block I) 2002 50 B [27553] 2002 Oct 30.13 2.1 days 2002 Nov 1.2 Cylinder 2400? 8.1 long 2.66 dia 2002 Oct 30.12 2002 Nov 1.02 51.62 51.62 88.75 6591 87.45 6527 195 144 230 152 0.003 0.0006 79 102 Eutelsat W5 [Delta-4M+4,2] 2002 51 A [27554] CC=LC37B 2002 Nov 20.94 > million years Box +2 panels 3170 1900 bol 1400 dry 4.6 x 2.5 x 1.8 29 span 2002 2002 2002 2002 2002 2002 2002 2002 2003 2012 20.74 22.70 24.56 1.90 2.90 4.94 15.81 16.68 6.70 19.97 13.62 8.52 2.77 0.15 0.11 0.11 0.10 0.08 0.04 0.05 637.93 721.85 1016.67 1437.32 1436.45 1436.12 1434.63 1431.18 1436.08 1436.08 24548 26656 33493 42189 42172 42165 42136 42069 42165 42165 562 4801 18425 35498 35786 35780 35378 35672 35731 35766 35777 35753 35803 36122 35800 35793 36137 35707 35841 35806 0.717 0.581 0.259 0.0007 0.0002 0.0002 0.009 0.0004 0.001 0.0005 181 181 181 45 118 204 94 125 309 23 Delta-4M+4,2 2nd stage 2002 51 B [27555] 2002 Nov 20.94 Cylinder 2850 12.00 long 2.44 dia 2002 Nov 20.76 2002 Nov 21.18 2012 Jan 19.86 13.14 13.44 13.95 615.70 612.53 611.92 23974 23892 23876 556 511 506 34635 34515 34489 0.711 0.712 0.712 178 179 198 Fragments 2002 51 C-K 8 pieces, all have decayed * Nov Nov Nov Dec Dec Dec Dec Dec Jan Jan For orbital information see extra pages at end of year Crew of 3 cosmonauts (Zalyotin, De Winne and Lonchakov) docked 2002 Nov 1.209 with ISS (PIRS); crew returned with Soyuz-TM 34. Soyuz-TMA1 undocked 2003 May 3.947 with Exp-6 crew (Bowersox, Budarin and Pettit). 2014-version 1.13 Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Size (m) Lifetime Date of orbital determination Orbital Inclination (deg) Nov Nov Nov Nov Nov Nov Nov Nov Nov Nov Dec Dec Dec Dec Dec Nodal period (min) Page 2002 -22 Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) D STS-113 # 7M Endeavour F19 R [Shuttle] 2002 52 A [27556] CC-LC39A 2002 Nov 24.035 13.783 days 2002 Dec 7.818 Delta wing 116460 ↑ 91498 ↓ 37.5 long 5.5 dia 23.8 span 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 24.06 24.16 24.75 25.73 25.92 26.25 26.58 26.92 27.58 27.73 1.58 1.77 6.17 6.58 7.44 51.63 51.64 51.64 51.64 51.63 51.64 51.63 51.63 51.63 51.64 51.64 51.64 51.63 51.64 51.63 89.98 91.12 91.83 92.20 92.32 92.30 92.30 92.30 92.30 92.40 92.40 92.50 92.43 92.43 92.42 6652 6708 6743 6761 6767 6766 6766 6766 6766 6770 6771 6776 6772 6772 6772 232 312 342 371 379 378 378 378 378 386 387 395 390 389 389 314 346 387 393 397 397 397 396 396 398 397 399 398 398 397 0.006 0.003 0.003 0.002 0.001 0.001 0.001 0.001 0.001 0.0009 0.0007 0.0003 0.0006 0.0006 0.0006 181 335 102 148 178 179 180 182 183 187 200 219 263 268 274 D Mepsi 1 A+B $ 2002 52 B [27562] 2002 Nov 24.03 68 days 2003 Jan 31 Cube 2 0.10x0.10 x0.125 2002 Dec 2.92 2003 Jan 31.62 51.65 51.63 92.42 88.25 6771 6567 388 184 397 192 0.0006 0.0005 207 144 D Astra 1K % [Proton-K] 2002 53 A [27557] BAI 2002 Nov 25.96 14.12 days 2002 Dec 10.08 Box+ 2 panels 2002 2002 2002 2002 2002 2002 26.20 26.87 27.12 27.73 30.30 10.02 51.57 51.57 51.59 51.60 51.60 51.63 88.18 88.07 88.95 90.22 90.23 90.12 6563 6557 6601 6663 6664 6659 175 171 146 279 276 209 193 186 299 290 295 352 0.001 0.001 0.012 0.0008 0.001 0.011 166 167 298 250 255 334 D Proton-K 4th stage (Block-DM3) 2002 53 B [27558] 2002 Nov 25.96 2.7 days 2002 Nov 28.6 Cylinder 2350? 6.22 long 3.7 dia 2002 Nov 26.20 2002 Nov 28.51 51.57 51.58 88.03 87.02 6556 6505 172 120 183 133 0.0009 0.001 261 202 ALSat 1 [Kosmos-3M] 2002 54 A [27559] PLE 2002 Nov 28.25 Cube + grav. boom 80 0.61 side 6 long 2002 Nov 28.31 2003 Apr 27.35 2012 Jan 20.78 98.23 98.22 97.81 99.02 98.48 97.97 7090 7064 7040 681 677 645 742 695 677 0.004 0.001 0.002 73 294 208 Mozhayets 2002 54 B [27560] 2002 Nov 28.25 Cylinder 80 0.80 high 0.75 dia 2002 Nov 28.31 2002 Nov 28.86 2012 Jan 20.81 98.24 98.24 97.94 99.03 99.07 98.93 7091 7093 7086 683 683 676 742 746 738 0.004 0.004 0.004 78 76 137 Nov Nov Nov Nov Nov Dec 2002 54 continued on next page # $ % Crew of 7 astronauts (Wetherbee, Lockhart, Lopez-Alegria, Herrington, Bowersox, Budarin and Pettit) docked with ISS (Destiny/PMA-2 port) 2002 Nov 26.916; undocked 2002 Dec 6.36. Installation of the P1-truss. Bowersox, Budarin and Pettit formed Expedition 6; Korzun Treschyov and Whitson Micro Electro-mechanical systems-based PicoSat Inspector released from cargo bay 2002 Dec ???; two cube picosats with a 15.2 m tether. Malfunction of Proton-K 4th stage left the satellite in a low earth orbit 2014-version 1.13 Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Size (m) Lifetime Date of orbital determination Orbital Inclination (deg) Cylinder 1435 6.00 long 2.40 dia 2002 Nov 28.31 2002 Nov 28.38 2012 Jan 20.07 98.24 98.24 97.97 2003 2005 2012 2003 2005 2012 Apr Feb Jan Apr Feb Jan 20.17 19.17 20.41 20.67 19.15 20.44 98.23 98.15 97.95 98.23 98.15 97.91 Dec Dec Dec Dec Dec Dec Dec Dec Dec Dec Jan Jan Feb Jul Jul Oct Nov Nov Jan Nodal period (min) Page 2002 -23 Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) 7094 7095 7090 686 686 678 744 747 745 0.004 0.004 0.005 81 81 177 7094 7090 7083 7088 7084 7076 687 682 676 678 674 668 745 741 733 741 736 727 0.004 0.004 0.004 0.004 0.004 0.004 343 69 133 353 76 110 Kosmos-3M 2nd stage (Rubin 3) 2002 54 C [27561] 2002 Nov 28.25 Fragments 2002-54 D [27768] 2002-54 E [27769] TDRS 10 [Atlas-2A] 2002 55 A [27566] CC 2002 Dec 5.11 2002 2002 2002 2002 2002 2002 2002 2002 2002 2002 2003 2003 2003 2004 2004 2004 2004 2004 2012 4.96 6.75 7.63 9.80 12.20 13.19 14.04 15.57 16.50 18.47 22.52 25.41 22.29 8.46 13.30 2.24 15.91 21.80 28.57 26.96 26.30 26.22 18.16 10.56 8.06 7.22 7.01 7.01 7.01 6.92 6.91 6.85 5.63 5.62 5.42 5.31 5.29 1.23 548.88 552.65 636.45 721.50 996.80 1227.02 1398.22 1436.78 1436.12 1436.10 1435.92 1436.25 1436.08 1435.92 1432.88 1432.80 1433.03 1436.07 1436.10 22207 22308 24510 26647 33055 37966 41420 42178 42165 42165 42161 42168 42164 42161 42102 42100 42105 42164 42165 219 431 427 4752 17567 27386 34291 35788 35762 35760 35762 35776 35773 35769 35707 35704 35709 35768 35730 31437 31429 35835 35786 35785 35788 35792 35812 35811 35813 35803 35803 35799 35796 35740 35739 35744 35803 35842 0.703 0.695 0.722 0.582 0.276 0.111 0.018 0.0003 0.0006 0.0006 0.0005 0.0003 0.0003 0.0003 0.0004 0.0004 0.0004 0.0004 0.001 176 177 178 179 179 178 177 327 320 329 351 3 31 156 188 258 280 304 197 Atlas-2A 2nd stage (Centaur) 2002 55 B [27567] 2002 Dec 5.11 2002 Dec 4.96 2012 Jan 27.35 26.94 26.88 545.42 304.33 22113 14988 211 225 31258 16993 0.702 0.559 175 348 Adeos 2 (Midori 2) [H-2A] 2002 56 A [27597] TAN 2002 Dec 14.06 2002 2002 2002 2012 14.25 19.23 19.72 27.73 98.69 98.69 98.69 98.35 100.98 101.00 100.98 100.95 7184 7184 7184 7182 805 804 805 802 805 807 806 805 0.00006 0.0002 0.00009 0.0002 87 326 299 35 Fedsat 2002 56 B [27598] 2002 Dec 14.06 2002 Dec 14.39 2012 Jan 28.82 98.67 98.26 100.85 100.82 7178 7176 792 792 806 803 0.0009 0.0008 32 296 2002 56 continued on next page 2014-version 1.13 Dec Dec Dec Jan 99.08 99.12 99.02 99.10 99.02 98.87 98.97 98.88 98.72 Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Date of orbital determination Orbital Inclination (deg) Nodal period (min) Page 2002 -24 Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) WEOS $ 2002 56 C [27599] 2002 Dec 14.06 2002 Dec 14.39 2012 Jan 28.14 98.68 98.27 100.82 100.78 7176 7174 790 789 805 802 0.002 0.0009 25 309 Micro-Labsat 2002 56 D [27600] 2002 Dec 14.06 2002 Dec 14.32 2012 Jan 28.87 98.67 98.27 100.80 100.77 7175 7173 789 787 804 802 0.001 0.001 44 309 H-2A 2nd stage 2002 56 E [27601] 2002 Dec 14.06 2002 Dec 14.32 2012 Jan 28.86 98.72 98.53 100.68 100.62 7169 7167 737 736 844 841 0.007 0.007 64 348 Rite Target 1 2002 56 F [28454] 2002 Dec 14.06 2004 Oct 28.98 2012 Jan 28.36 98.71 98.30 100.75 100.68 7173 7169 787 784 802 798 0.001 0.001 174 303 Rite Target 2 2002 56 G [28455] 2002 Dec 14.06 2004 Oct 30.40 2012 Jan 28.92 98.60 98.30 100.77 100.68 7173 7169 787 784 802 798 0.001 0.001 174 308 NSS 6 [Ariane-44L] (V156 #115) 2002 57 A [27603] KOU-ELA2 2002 Dec 17.96 > million years Box+ 2 panels 4575 3.62x3.62 x7.3 2002 2002 2002 2002 2002 2002 2002 2002 2003 2012 17.77 19.07 20.01 20.24 22.09 24.20 26.35 30.57 1.29 27.55 6.98 5.31 4.42 4.34 2.07 0.97 0.06 0.06 0.06 0.05 630.80 673.75 706.82 711.75 882.17 1077.92 1431.82 1435.93 1436.10 1436.08 24364 25458 26285 26407 30469 34825 42081 42162 42165 42165 222 2421 4079 4316 12460 21168 35668 35749 35777 35773 35749 35738 35733 35741 35722 35724 35737 35817 35795 35799 0.729 0.654 0.602 0.595 0.382 0.209 0.0008 0.0008 0.0002 0.0003 178 179 179 179 179 179 195 45 21 40 Ariane-4 3rd stage (H-10-3)+VEB 2002 57 B [27604] 2002 Dec 17.96 Cylinder 1670 Cylinder 11.05 long 2.6 dia 1.03x4.0 2002 Dec 17.75 2002 Dec 18.21 2012 Jan 28.21 6.92 7.22 7.81 659.23 660.70 631.15 25091 25128 24698 218 298 292 37207 37201 35698 0.737 0.734 0.726 178 179 270 Rubin 2 [Dnepr] 2002 58 A [27605] BAI 2002 Dec 20.71 2002 Dec 20.77 2002 Dec 20.84 2012 Jan 29.02 64.57 64.58 64.56 97.95 97.83 97.75 7039 7034 7030 633 631 592 689 679 711 0.004 0.003 0.008 134 140 276 LatinSat-B 2002 58 B [27606] 2002 Dec 20.71 2002 2002 2002 2012 64.55 64.56 64.56 64.56 98.07 98.05 98.08 97.95 7045 7044 7045 7040 631 626 632 595 701 705 701 727 0.005 0.006 0.005 0.009 131 128 134 280 2002 58 continued on next page $ Size (m) Lifetime Whale Ecology Observation Satellite 2014-version 1.13 Dec Dec Dec Dec Dec Dec Dec Dec Jan Jan Dec Dec Dec Jan 20.75 21.93 22.74 28.29 Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Date of orbital determination Orbital Inclination (deg) 2002 2002 2002 2012 2002 2002 2012 21.04 21.18 21.52 28.91 20.77 21.17 27.73 64.55 64.56 64.56 64.96 64.87 64.56 64.56 97.87 97.97 97.97 97.80 96.30 97.75 97.62 Size (m) Lifetime Page 2002 -25 Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) 7035 7040 7040 7032 6960 7030 7023 634 633 632 594 293 636 596 679 690 691 713 869 667 693 0.003 0.004 0.004 0.009 0.041 0.002 0.007 136 135 137 276 237 134 268 Saudisat-1C 2002 58 C [27607] 2002 Dec 20.71 Unisat 2 2002 58 D [27608] 2002 Dec 20.71 Trailblazer 2 2002 58 E [27609] 2002 Dec 20.71 2002 Dec 20.77 2002 Dec 21.17 2012 Jan 28.23 64.51 64.56 64.56 96.32 97.55 97.48 6961 7020 7017 405 638 600 759 645 677 0.025 0.0005 0.005 233 132 258 Dnepr ??? stage 2002 53 F [27610] 2002 Dec 20.71 2002 Dec 20.91 2012 Jan 28.91 64.56 64.55 100.92 100.88 7181 7179 599 584 1005 1016 0.028 0.030 136 349 Gas shield (PLEM Cover) 2002 53 G [27611] 2002 Dec 20.71 2002 Dec 21.04 2002 Dec 21.17 2012 Jan 27.87 64.85 64.56 64.54 96.93 97.45 96.83 6990 7016 6986 522 633 577 701 640 637 0.013 0.0005 0.004 23 331 252 LatinSat-A 2002 58 H [27612] 2002 Dec 20.71 2002 2002 2002 2012 Dec Dec Dec Jan 20.77 22.50 31.96 28.20 64.61 64.56 64.56 64.56 95.88 97.55 97.65 97.52 6939 7020 7025 7018 476 638 637 597 646 645 655 683 0.012 0.0005 0.001 0.006 327 111 127 263 Cosmos 2393 [ ] 2002 59 A [27613] PLE 2002 Dec 24.51 2002 2003 2003 2012 Dec Jan Jan Jan 24.57 5.86 12.79 27.40 62.84 62.87 62.85 64.72 704.62 715.92 718.18 719.18 26230 26510 26566 26590 517 538 548 1172 39186 39723 39826 39252 0.737 0.739 0.739 0.716 287 287 287 248 D ??? stage 2002 59 B [27614] 2002 Dec 24.51 41 days 2003 Feb 3 2002 Dec 24.63 2003 Feb 3.25 62.81 62.78 92.10 87.08 6756 6508 227 120 528 139 0.022 0.001 114 115 D ??? platform 2002 59 C [27615] 2002 Dec 24.51 22 days 2003 Jan 15 2002 Dec 24.69 2003 Jan 15.39 62.84 62.82 91.90 6746 87.57 6532 196 134 538 173 0.025 0.003 115 110 ??? stage 2002 59 D [27616] 2002 Dec 24.51 2002 Dec 24.57 2012 Jan 27.60 62.84 64.83 701.62 26156 701.55 26154 516 1932 39038 37618 0.736 0.682 287 258 2014-version 1.13 Dec Dec Dec Jan Dec Dec Jan Nodal period (min) Year of Launch 2002 Name [Launcher] Fragment Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Date of orbital determination Orbital Inclination (deg) Size (m) Lifetime Nodal period (min) Page 2002 -26 Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) Cosmos 2394 * [Proton-K / Block DM-2] 2002 60 A 2002 Dec 25.32 [27617] BAI-LC81/23 Cyl+ 2 panels+ 2.4 dia magnometerboom 3.7 height 1370 2002 2002 2002 2003 2003 2012 Dec Dec Dec Jan Jan Jan 25.33 25.66 26.81 5.41 7.55 28.27 64.77 64.77 64.79 64.79 64.79 64.76 675.63 675.78 675.68 676.43 675.73 675.72 25506 25509 25507 25526 25508 25508 19123 19125 19122 19124 19122 19125 19131 19137 19134 19171 19136 19134 0.0002 0.0002 0.0002 0.0009 0.0003 0.0002 154 199 110 59 144 127 Cosmos 2396 * 2002 60 B [27618] 2002 Dec 25.32 Cyl+ 2 panels+ 2.4 dia magnometerboom 3.7 height 1370 2002 2003 2003 2003 2012 Dec Jan Jan Jan Jan 27.20 5.72 14.54 18.49 27.23 64.80 64.79 64.77 64.79 64.76 675.65 679.80 676.68 675.73 675.73 25506 25610 25532 25508 25508 19124 19129 19115 19101 19090 19131 19335 19192 19158 19169 0.0001 0.004 0.002 0.001 0.002 227 71 102 151 148 Cosmos 2395 * 2002 60 C [27619] 2002 Dec 25.32 Cyl+ 2 panels+ 2.4 dia magnometerboom 3.7 height 1370 2002 2002 2003 2003 2003 2003 2012 Dec Dec Jan Jan Jan Feb Jan 26.74 27.65 4.30 13.00 13.92 7.10 27.27 64.80 64.79 64.80 64.80 64.79 64.79 64.77 675.72 675.70 671.60 673.88 975.73 675.72 675.72 25508 25508 25404 25462 25508 25508 25508 19120 19120 18917 19028 19115 19114 19113 19139 19138 19134 19138 19145 19145 19145 0.0004 0.0004 0.004 0.002 0.0006 0.0006 0.0006 201 202 243 248 312 312 277 Proton-K 4th stage (Block DM-2) 2002 60 D [27620] 2002 Dec 25.32 Cylinder 2350? 6.22 long 3.7 maxdia 2002 Dec 25.33 2012 Jan 27.55 64.78 64.76 674.65 25481 674.62 25480 19077 19095 19128 19108 0.001 0.0003 286 227 D Proton-K Ullage motor 2002 60 E [27621] 2002 Dec 25.32 2327 days 2009 May 9 Cylinder 55 0.90 long 0.68 dia 2003 Jan 2.64 2003 Jan 3.59 2009 May 9.43 64.83 64.84 63.89 340.15 16142 340.17 16142 87.82 6545 394 394 81 19133 19133 252 0.580 0.580 0.013 297 297 204 D Proton-K Ullage motor 2002 60 F [27622] 2002 Dec 25.32 2421 days 2009 Aug 11 Cylinder 55 0.90 long 0.68 dia 2003 Jan 2.64 2009 Aug 10.52 64.76 63.87 340.17 16142 89.85 6646 392 99 19135 435 0.581 0.025 297 202 D Shen Zou 4 [CZ-42F] 2002 61 A [27630] JIUQ 2002 Dec 29.49 7 days 2003 Jan 5 2002 2002 2002 2003 Dec Dec Dec Jan 29.99 30.93 31.02 5.47 42.41 42.41 42.41 42.41 89.80 89.70 91.20 91.20 6643 6638 6712 6712 198 195 330 330 331 325 336 336 0.010 0.010 0.0004 0.0004 131 139 170 219 D CZ-4F 2nd stage 2002 61 B [27631] 2002 Dec 29.49 11 days 2003 Jan 9 2002 2002 2002 2002 2002 2003 Dec Dec Dec Dec Dec Jan 29.99 30.297 30.298 31.32 31.05 9.44 42.42 42.44 42.40 42.42 42.41 42.39 89.57 87.72 87.98 88.37 89.70 87.70 6632 6540 6553 6572 6638 6539 190 146 155 131 195 138 317 177 194 257 324 183 0.010 0.002 0.003 0.010 0.010 0.003 122 142 151 125 140 224 2002 61 continued on next page * Triple Glonass payload; two are Glonass-M sats 2014-version 1.13 Year of Launch 2002 Name [Launcher] Fragment D Cospar ID Launch date [Norad#] Launchsite Lifetime and descent date Cospar ID [Norad#] RAE Table of Earth Satellites (Compiled 2007) Shape and weight (kg) Descent date Date of orbital determination Orbital Inclination (deg) Size (m) Lifetime Nodal period (min) Page 2002 -27 Semi major axis (km) Perigee height (km) Apogee height (km) Orbital Argument eccentricity of perigee (deg) Orbital module 2002 61 C [27634] 2002 Dec 29.49 254 days 2003 Sep 9 2002 2003 2003 2003 2003 2003 2003 2003 2003 2003 2003 Dec Jan Jan Jan Feb Feb Mar Mar Apr Apr Sep 30.33 5.60 5.71 5.84 9.64 9.90 1.92 2.18 16.97 17.80 9.17 42.41 42.41 42.43 42.41 42.42 42.42 42.42 42.41 42.42 42.41 42.40 91.20 91.22 91.60 91.73 91.30 91.78 91.57 91.78 91.30 91.63 87.25 6712 6713 6732 6738 6717 6741 6730 6740 6717 6733 6517 330 330 344 354 331 359 351 351 331 344 128 337 338 362 366 346 365 352 372 345 365 149 0.0005 0.0006 0.001 0.0009 0.001 0.0005 0.00008 0.002 0.001 0.002 0.002 164 249 243 192 74 282 265 307 255 126 301 Nimiq 2 [Proton-M / Breeze-M] 2002 62 A [27632] BAI 2002 Dec 29.97 > million years 2002 2002 2002 2003 2003 2003 2003 2003 2003 2003 2003 2003 2003 2003 2003 2003 2003 2003 2012 Dec Dec Dec Jan Jan Jan Jan Jan Jan Jan Jan Jan Feb Feb Mar Mar Mar Mar Jan 30.02 30.47 31.55 2.48 6.44 6.93 8.11 10.19 16.23 22.71 28.94 30.40 6.70 27.73 2.82 4.20 5.71 6.73 27.72 48.99 16.49 8.57 3.79 0.10 0.10 0.09 0.07 0.05 0.05 0.05 0.06 0.05 0.05 0.05 0.03 0.05 0.04 0.06 645.57 788.57 928.38 1119.47 1432.90 1435.72 1436.33 1435.97 1436.07 1441.03 1436.85 1436.50 1436.08 1428.87 1427.30 1435.25 1436.10 1436.08 1436.10 24743 28274 31525 35714 42102 42157 42170 42162 42164 42261 42180 42173 42165 42023 41992 42148 42165 42165 42165 946 7904 14551 22922 35677 35763 35787 35779 35779 35827 35775 35763 35779 35520 35515 35769 35778 35778 35770 35783 35886 35740 35748 35770 35794 35795 35789 35793 35938 35827 35825 35793 35768 35713 35771 35795 35794 35803 0.704 0.495 0.336 0.180 0.001 0.0004 0.0001 0.0001 0.0002 0.001 0.0006 0.0007 0.0002 0.003 0.002 0.00003 0.0002 0.0002 0.0004 0 359 0 0 201 79 37 355 35 234 26 26 169 45 20 246 61 60 51 Proton-M 4th stage (Breeze-M) 2002 62 B [27633] 2002 Dec 29.97 Cylinder 1220 2.62 long 2.4 dia 2003 Jan 2.24 2012 Jan 28.22 16.41 15.22 783.72 28158 783.70 28158 7873 8102 35686 35456 0.494 0.486 359 223 Breeze-M APT 2002 62 C [27646] 2002 Dec 29.97 Torus 1290 2.1 long 4.1 dia 0.8 cross 2003 Jan 15.28 2012 Jan 28.62 49.51 49.51 312.12 15242 312.05 15240 612 574 17115 17149 0.541 0.544 357 293 2014-version 1.13 Year of Launch 2002 Cospar ID [Norad number] RAE Table of Earth Satellites (Compiled 2005) Descent date Date of orbital Determination Lifetime Extra Page 2002 -1 Orbital Inclination (deg) Nodal period (min) Semi major axis (km) Perigee height (km) Apogee height (km) Orbital eccentric. Argument of perigee (deg) Text in box is from "History of on-orbit satellite fragmentations", 13th edition, May 2004. Orbital Debris Program Office, Johnson Space Centre, NASA, Houston, TX 77058. Iridium 2002 2002 2002 2002 91 05 05 05 05 fragments; 4 pieces, all in orbit G [40324] H [40325] J [40326] K [40327] Hai Yang 1/Feng Yun-1 4 CZ-4B 3rd stage fragment; 7 pieces, in orbit. Fragment D may be the payload adapter. 2002-24 D [27433] 2002-24 E [28438] 2002-24 F [29215] 2002-24 G [29216] 2002-24 H 2002-24 J 2002-24 K [34223] [35404] [35405] Cosmos 2390/2391 fragments; 2 pieces, both in orbit 2002 36 D [27533] 2002 36 E [27546] Cosmos 2392 2002-37 2002-37 Cosmos 2392 D 2002-37 D 2002-37 D 2002-37 fragments; 2 pieces, both in orbit G [27476] H [27494] Proton-K ullage motor 1 fragments; 58 pieces, 51 have decayed J [28689] 2005 Jun 3 1044 days K [28690] 2005 Jun 4 1045 days L [28691] 2005 Jun 4 1045 days D D 2002-37 2002-37 M N [28692] [28693] 2005 Jun 6 2005 Jun 15 1047 days 1056 days D D D D D 2002-37 2002-37 2002-37 2002-37 2002-37 P Q R S T [28705] [28715] [28716] [28717] [28718] 2005 2005 2005 2005 2005 1071 1071 1071 1071 1071 2014-version 1.13 Jun Jun Jun Jun Jun 30 30 30 30 30 days days days days days 2002 2002 2002 2002 Dec Dec Dec Dec 3.65 3.61 3.68 3.69 86.45 86.42 86.45 86.40 101.12 99.53 99.72 99.97 7190 7115 7123 7135 723 697 696 734 900 775 793 779 0.012 0.005 0.007 0.003 298 40 95 46 2002 2005 2012 2004 2005 2012 2006 2012 2006 2012 2009 2009 2009 May Feb Jun Sep Feb Jan Jun Jan Jun Jan Feb Jun Jun 15.27 19.18 9.97 26.66 19.08 8.31 5.23 7.23 5.01 5.37 27.45 17.22 19.45 98.81 98.68 98.71 98.73 98.73 98.50 98.83 98.82 98.88 98.82 98.78 98.48 98.61 102.15 102.12 102.05 101.35 101.33 101.12 105.83 105.78 105.45 105.40 102.92 101.48 102.10 7239 7237 7234 7201 7200 7190 7412 7410 7394 7392 7275 7207 7237 850 848 846 805 804 793 847 846 844 842 793 789 762 870 869 866 841 840 830 1219 1217 1186 1184 999 868 955 0.001 0.001 0.001 0.003 0.002 0.003 0.025 0.025 0.023 0.023 0.014 0.005 0.013 194 216 271 28 322 224 276 354 255 302 194 24 106 2002 2005 2012 2002 2005 2012 Sep Feb Jan Oct Feb Jan 25.69 15.36 13.58 23.64 19.80 14.52 82.49 82.49 82.48 82.49 82.48 82.48 115.70 115.70 115.68 115.67 115.67 115.65 7866 7865 7865 7864 7864 7864 1466 1468 1469 1463 1466 1468 1508 1505 1503 1508 1505 1502 0.003 0.002 0.002 0.003 0.002 0.002 128 18 252 69 14 251 2005 Feb 19.77 2005 Feb 19.50 63.46 63.48 119.83 8052 118.98 8014 1468 1472 1879 1799 0.025 0.020 356 353 2005 2005 2005 2005 2005 2005 2005 2005 3.41 3.29 3.95 4.40 2.17 6.20 14.14 30.13 63.45 63.46 63.64 63.63 63.80 63.44 63.43 63.65 92.28 94.03 93.95 92.90 95.05 94.87 92.55 91.53 6765 6851 6847 6795 6900 6891 6778 6728 234 264 298 287 266 281 263 259 540 679 638 546 775 744 536 440 0.023 0.030 0.025 0.019 0.037 0.034 0.020 0.013 144 137 140 145 142 143 147 138 2005 Jun 30.15 2005 Jun 30.17 2005 Jun 30.07 63.66 63.65 63.66 94.12 6854 95.58 6925 91.77 6740 262 265 212 689 828 511 0.031 0.041 0.022 123 121 130 Jun Jun Jun Jun Jun Jun Jun Jun Year of Launch 2002 Cospar ID [Norad number] RAE Table of Earth Satellites (Compiled 2005) Descent date Date of orbital Determination Orbital Inclination (deg) 2005 Jun 29.94 63.65 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2006 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2006 2005 2005 2005 63.48 63.57 63.55 63.66 63.74 63.70 63.69 63.70 63.67 63.73 63.73 63.67 63.23 63.60 63.59 63.34 63.28 63.39 63.36 63.62 63.59 63.77 63.76 63.32 63.28 63.55 63.53 63.71 63.69 63.79 63.77 63.94 63.93 64.05 64.01 63.71 63.68 63.30 63.74 63.94 63.91 63.40 63.30 63.11 63.09 63.62 D D D D 2002-37 2002-37 2002-37 2002-37 U V W X [28719] [28720] [28721] [28722] 2005 2005 2005 2005 D D 2002-37 2002-37 Y Z [28723] [28724] 2005 Jun 30 2005 Jul 28 1071 days 1099 days D 2002-37 AA 2002-37 AB [28725] [28726] 2005 Aug 17 1119 days D 2002-37 AC 2002-37 AD [28727] [28728] 2005 Aug 2 1104 days D 2002-37 AE 2002-37 AF [28729] [28730] 2005 Sep 5 1138 days D 2002-37 AG [28731] 2006 Jan 7 1262 days D 2002-37 AH [28732] 2005 Oct 5 1168 days D 2002-37 AJ [28733] 2005 Oct 7 1170 days D 2002-37 AK [28734] 2005 Oct 3 1166 days D 2002-37 AL [28735] 2005 Oct 3 1166 days D 2002-37 AM [28736] 2005 Sep 28 1161 days D 2002-37 AN [28743] 2005 Nov 4 1198 days D 2002-37 AP [28744] 2005 Oct 11 1164 days D 2002-37 AQ [28745] 2005 Aug 27 1129 days D 2002-37 AR [28746] 2005 Aug 2 1104 days D 2002-37 AS [28747] 2005 Jul 12 1083 days D D 2002-37 AT 2002-37 AU 2002-37 AV [28748] [28749] [28750] 2005 Jul 10 2005 Dec 11 1081 days 1235 days D 2002-37 AW [28751] 2006 Apr 30 1373 days 2002-37 AX 2002-37 AY 2002-37 AZ [28752] [28753] [28754] 2014-version 1.13 Jun Jun Jul Jul Lifetime 30 30 4 7 1071 1071 1075 1078 days days days days Jun Jul Jul Jun Jul Jul Jul Jul Aug Jul Jul Aug Jul Jul Sep Jul Jan Jul Oct Jul Oct Jul Oct Jul Oct Jul Sep Jul Nov Jul Sep Jul Aug Jul Aug Jul Jul Jul Jul Jul Dec Jul Apr Jul Jul Jul 30.02 1.99 7.15 30.00 1.41 27.70 1.42 1.16 16.45 1.16 2.00 1.72 2.10 2.12 5.17 2.18 6.36 1.91 4.95 1.93 7.35 1.93 1.87 1.69 3.83 2.07 27.85 7.93 4.04 7.98 27.61 7.97 25.06 7.95 2.54 7.88 10.88 8.03 7.92 7.96 10.98 8.04 30.46 7.95 7.93 7.92 Extra Page 2002 -2 Nodal period (min) Semi major axis (km) 92.60 6781 94.82 94.32 90.70 92.45 95.18 88.68 95.77 96.32 88.78 96.95 94.90 88.75 97.30 97.72 88.78 98.23 88.75 101.23 90.00 94.80 89.47 94.45 88.63 100.75 89.48 95.20 89.65 95.48 89.45 94.50 88.50 93.52 89.30 95.60 89.98 91.73 90.50 96.97 93.57 97.08 88.08 95.42 87.75 95.93 96.67 99.00 6888 6864 6688 6773 6906 6588 6934 6961 6593 6991 6893 6592 7008 7028 6593 7053 6591 7196 6653 6887 6626 6871 6585 7173 6627 6907 6636 6921 6626 6873 6579 6825 6619 6926 6652 6738 6678 6992 6827 6997 6558 6917 6542 6943 6978 7089 Perigee height (km) Apogee height (km) Orbital eccentric. Argument of perigee (deg) 277 527 0.018 129 309 301 266 277 253 179 263 270 184 421 238 183 296 271 188 283 192 302 226 332 231 238 180 308 214 339 232 260 203 229 170 221 183 300 239 238 211 290 200 249 160 284 159 320 295 425 709 670 352 512 803 240 848 893 244 804 790 242 962 1028 241 1066 234 1332 323 685 265 746 234 1280 283 718 282 824 291 759 230 672 297 796 307 481 387 937 697 989 198 792 167 808 903 996 0.029 0.027 0.006 0.017 0.040 0.005 0.042 0.045 0.005 0.027 0.040 0.004 0.047 0.054 0.004 0.056 0.003 0.072 0.007 0.026 0.003 0.037 0.004 0.068 0.005 0.027 0.004 0.041 0.007 0.039 0.005 0.033 0.009 0.035 0.005 0.018 0.013 0.046 0.036 0.053 0.003 0.037 0.0006 0.035 0.044 0.040 121 122 121 129 130 118 126 122 109 137 133 120 137 118 108 137 99 106 100 120 91 115 96 105 103 115 101 126 98 115 98 108 97 147 136 107 100 135 118 123 89 128 86 140 136 129 Year of Launch 2002 Cospar ID [Norad number] RAE Table of Earth Satellites (Compiled 2005) Descent date Lifetime Date of orbital Determination Orbital Inclination (deg) 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2006 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2005 2013 2005 2005 2005 2005 2005 2005 2005 Jul Nov Jul Aug Jul Oct Jul Dec Jul Jul Jul Jul Jul Jul Jul Jul Jul May Jul Oct Jul Aug Jul Sep Jul Jul Jul Aug Jul Jul Apr Jul Jul Aug Sep Sep Sep Nov 7.91 24.88 7.98 3.24 7.95 9.56 7.96 19.57 7.94 22.60 7.93 17.75 8.03 13.81 7.95 27.72 7.90 18.06 7.97 23.85 8.02 20.12 8.03 15.12 7.87 15.03 7.93 18.09 7.96 7.99 25.44 7.86 7.80 5.49 6.40 17.64 7.88 3.61 62.61 62.45 63.93 63.91 63.45 63.40 63.24 63.20 63.40 63.17 63.75 63.72 64.59 64.59 63.43 63.41 63.35 63.28 63.38 63.35 63.78 63.78 63.89 63.88 63.68 63.71 63.57 63.55 63.64 63.28 63.23 63.63 63.51 63.46 63.17 63.16 62.94 62.89 95.35 88.38 93.43 87.53 99.05 88.85 99.22 88.62 92.13 87.73 93.87 92.23 94.25 89.12 95.38 89.55 98.30 88.37 99.33 89.80 94.05 89.38 94.28 88.92 93.28 89.65 99.48 89.68 93.48 95.60 88.58 97.42 93.88 89.83 92.90 89.97 95.07 89.67 2002 2002 2002 2002 2002 2002 2002 2002 Sep Dec Sep Nov Sep Nov Sep Oct 10.46 11.90 10.46 3.67 10.72 12.12 16.80 1.56 30.40 30.38 30.40 30.40 30.41 30.40 30.40 30.40 93.53 87.55 93.52 88.17 93.57 88.33 93.02 90.80 D 2002-37 BA [28755] 2005 Nov 25 1219 days D 2002-37 BB [28756] 2005 Aug 3 1105 days D 2002-37 BC [28757] 2005 Oct 9 1172 days D 2002-37 BD [28758] 2005 Dec 19 1243 days D 2002-37 BE [28759] 2005 Jul 22 1093 days D 2002-37 BF [28760] 2005 Jul 18 1089 days D 2002-37 BG [28761] 2005 Jul 13 1084 days D 2002-37 BH [28762] 2005 Jul 27 1098 days D 2002-37 BJ [28763] 2006 May 18 1393 days D 2002-37 BK [28764] 2005 Oct 24 1187 days D 2002-37 BL [28765] 2005 Aug 22 1124 days D 2002-37 BM [28766] 2005 Sep 16 1149 days D 2002-37 BN [28767] 2005 Jul 15 1086 days D 2002-37 BP [28768] 2005 Aug 18 1120 days D D 2002-37 BQ 2002-37 BR [28769] [28770] 2005 Jul 10 2013 Apr 27 1081 days 3929 days D 2002-37 BS 2002-37 BT [28771] [28772] 2005 Aug 5 1107 days D 2002-37 BU [28860] 2005 Sep 18 1151 days D 2002-37 BV [28861] 2005 Nov 4 1198 days Users/Kodama H-2A stage fragments; 4 pieces; all have decayed. D 2002-42 C [27517] 2002 Dec 11 92 days D 2002-42 E [27519] 2002 Nov 3 54 days D 2002-42 F [27520] 2002 Nov 12 63 days D 2002-42 G [27527] 2002 Oct 2 22 days 2014-version 1.13 Extra Page 2002 -3 Nodal period (min) Semi major axis (km) Perigee height (km) Apogee height (km) Orbital eccentric. Argument of perigee (deg) 6914 6573 6821 6530 7092 6596 7100 6585 6758 6541 6842 6763 6861 6609 6915 6630 7056 6572 7105 6643 6851 6622 6863 6599 6814 6635 7112 6637 6824 6926 6583 7013 6843 6645 6795 6651 6900 6637 300 181 210 137 321 190 314 191 291 59 217 216 195 169 254 200 275 180 329 229 241 195 234 192 237 189 227 210 208 296 194 265 344 250 268 223 295 228 770 209 674 167 1105 245 1128 222 468 266 710 552 768 292 819 304 1080 207 1124 299 703 292 734 250 633 325 1190 307 682 799 214 1004 586 283 564 323 748 289 0.034 0.002 0.034 0.002 0.055 0.004 0.057 0.002 0.013 0.016 0.036 0.025 0.042 0.009 0.041 0.008 0.057 0.002 0.056 0.005 0.034 0.007 0.036 0.004 0.029 0.010 0.064 0.007 0.035 0.036 0.001 0.053 0.018 0.002 0.022 0.008 0.033 0.005 136 181 104 91 104 107 148 148 106 345 130 132 117 116 115 100 132 153 102 88 113 108 111 101 132 127 110 104 121 131 12 132 112 77 110 114 146 137 6826 6531 6825 6563 6828 6570 6801 6693 439 150 440 182 442 184 414 306 455 156 453 186 456 199 430 322 0.001 0.0004 0.0009 0.0003 0.001 0.001 0.001 0.001 281 196 289 276 271 47 320 99 Year of Launch 2002 Cospar ID [Norad number] RAE Table of Earth Satellites (Compiled 2005) Descent date Date of orbital Determination Orbital Inclination (deg) 2002 2002 2002 2002 2002 2002 2002 2002 Oct Nov Oct Oct Oct Oct Oct Oct 24.78 1.30 24.63 30.51 25.74 29.51 25.74 29.52 51.55 51.53 51.60 51.60 51.55 51.54 51.51 51.49 94.83 87.58 94.50 91.35 93.47 89.85 93.57 89.87 2004 2005 2010 2004 2005 2007 2004 2005 2011 2004 2005 2010 Sep Feb Dec Sep Feb Nov Sep Feb Apr Sep Feb Mar 27.02 20.01 7.79 25.39 19.93 21.56 29.04 18.54 17.79 26.05 19.56 29.82 97.26 97.22 97.28 97.37 97.29 97.16 97.33 97.31 97.33 97.30 97.28 97.18 2002 2002 2002 2002 2002 2002 2002 2003 2003 2003 2005 2006 2003 2003 2003 2005 2006 Nov Dec Dec Dec Dec Dec Dec Mar May Mar Feb Nov Mar Nov Mar Jan Jan 27.91 2.79 7.99 9.63 2.84 5.00 5.71 20.89 26.54 21.19 19.80 23.11 21.58 2.25 21.12 14.70 27.29 25.75 25.53 25.55 25.65 25.67 25.68 25.70 24.17 24.07 22.37 22.32 22.26 20.92 20.95 17.35 17.16 17.27 23.73 Lifetime Integral Proton-K fragment; 4 pieces, all have decayed. D 2002-48 E [27544] 2002 Nov 1.3 14.1 days D 2002-48 F [27547] 2002 Oct 31 14 days D 2002-48 G [27548] 2002 Oct 29 12 days D 2002-48 H [27549] 2002 Oct 29 12 days JB 3B CZ-4B stage fragments; 4 pieces, all have decayed. D 2002-49 C [28439] 2010 Dec 11 2938 days D 2002-49 D [28440] 2007 Nov 25 1855 days D 2002-49 E [28441] 2011 Apr 22 3099 days D 2002-49 F [28442] 2010 Mar 31 2712 days Eutelsat W5 Delta-4M2 (4) 2nd stage fragment; 8 pieces, all have decayed. D 2002-51 C [27563] 2002 Nov 30 10 days D 2002-51 D [27564] 2002 Dec 9 19 days D 2002-51 E [27565] 2002 Dec 6 16 days D 2002-51 F [27694] 2003 May 26 187 days D 2002-51 G [27695] 2006 Nov 29 1470 days D 2002-51 H [27696] 2003 Nov 6 351 days D 2002-51 J [27697] 2006 Jan 28 1165 days D 2002-51 K [27771] 2003 Apr 3 134 days 2014-version 1.13 Extra Page 2002 -4 Nodal period (min) Semi major axis (km) Perigee height (km) Apogee height (km) Orbital eccentric. Argument of perigee (deg) 6869 6533 6873 6719 6823 6646 6828 6646 189 127 188 170 182 157 183 158 832 182 800 511 706 377 715 378 0.047 0.004 0.045 0.025 0.038 0.017 0.039 0.017 117 136 106 125 104 124 110 123 93.05 95.78 88.92 95.27 94.88 90.15 96.03 95.78 90.47 95.72 95.25 89.78 6948 6935 6600 6910 6892 6658 6947 6935 6676 6932 6917 6642 458 453 213 449 436 268 457 451 279 445 446 258 681 660 229 614 590 290 679 662 315 661 631 270 0.016 0.015 0.001 0.012 0.011 0.002 0.016 0.015 0.003 0.016 0.013 0.0009 342 195 157 330 168 312 339 215 190 338 193 18 94.15 96.18 93.10 88.28 95.15 93.63 92.65 101.53 90.13 119.00 106.27 92.88 132.15 97.52 214.98 215.68 95.38 96.37 6856 6954 6805 6568 6904 6831 6783 7210 6660 8014 7432 6794 8594 7018 11888 11914 6916 376 423 349 158 392 346 317 448 266 542 471 392 566 303 504 1175 294 734 578 728 503 222 659 559 492 1214 295 2729 1635 439 8594 977 10514 9895 780 435 0.015 0.022 0.011 0.005 0.019 0.016 0.013 0.053 0.002 0.136 0.078 0.003 0.192 0.048 0.421 0.366 0.035 216 274 341 359 267 292 303 201 180 333 218 31 199 91 167 196 316
