grl53939-sup-0001-s01AA

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Supplement to “Forecasting and Remote Sensing Outer-belt Relativistic
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Electrons from Low-Earth-Orbit”
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Yue Chen, Geoffrey D. Reeves, Gregory S. Cunningham, Robert J. Redmon, and Michael
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Henderson
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Correspondence to: cheny@lanl.gov
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This supplement includes materials that are relevant but not essential to presenting the
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main conclusions. First we validate the chorus wave proxy using recent Van Allen Probes
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data, and then we examine measurements of >100 keV electrons from POES MEPED E2
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channel in detail. Next, by deriving pseudo POES data from pitch-angle resolved Van
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Allen Probes MagEIS observations and comparing to original POES data, we are able to
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confirm that the observed cross-energy cross-pitch-angle coherence is real and not due to
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MeV electron contamination on POES instruments. At last, we show how the electron
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phase space density radial distributions observed by Van Allen Probes vary over time and
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then evaluate the role of the magnetopause boundary and radial diffusion.
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1. Validation of the Chorus Wave Proxy Method
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The chorus wave proxy method developed in Chen et al. [2014a] is tested using long-term
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Van Allen Probes observations from 2012 Oct. to 2014 Dec. Besides confirming the one-
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to-one temporal correlation, we quantitatively validated the proxy method taking
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advantage of the two probes. Within each 4.5 h time bin, we first derive the fitting
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parameter P by comparing Van Allen Probe-A chorus wave observations to POES
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precipitation at the conjunctive (L, MLT) positions as defined by Equ (1) of Chen et al.
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[2014a], then validate the method by applying the same P parameter to POES data so as to
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compare with chorus wave observations from Probe-B at other conjunctive (L, MLT)
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positions. One such example is shown in Figure S1. Indeed, the PE value for Probe-A (i.e.,
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an in-sample test) is 0.37 and the PE for Probe-B (out-of-sample test) is 0.11 for this 3-
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month period. In comparison, PE values using empirical averaged, three-Kp categorized
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chorus distributions from CRRES data are ~ -1.2 for both satellites during the same period.
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2. POES E2 Measurements within the Period
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NOAA POES satellites have circular sun-synchronous orbits (altitude ~800-850 km,
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inclination ~98o) with a period of ~102 min. The Space Environment Monitor-2 (SEM-2)
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on board each 3-axis stabilized POES spacecraft contains 2 solid-state detector
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telescopes—one oriented to view in the anti-Earth-center direction (i.e., the 0o telescope)
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and the other to view at about 90o to the first (i.e., the 90o telescope)—to measure
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electrons in 3 energy ranges (E1, 0.03-2.5 MeV, E2, 0.1-2.5 MeV and E3, 0.3-2.5 MeV).
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Figure S2 presents details of NOAA-15 E2 (>100 keV) data during the period. Panel A
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replots the same ratio curve as in Figure 1E, and Panel B shows the count rates from the
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90o telescope (blue) compared to 1 MeV fluxes from MagEIS (red). The green vertical
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lines mark the spikes in Panel A, and it can be seen that the leading edge of each spike in
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Panel A always corresponds to a simultaneous increment in >100 keV electrons in Panel B,
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while significant dropouts of 1 MeV electrons may (e.g., events 3 and 9) or may not (e.g.,
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events 5 and 11) be coincidental. By comparing the timings and amplitudes of both
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increments and dropouts, we conclude that it is the increments of >100 keV precipitation
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instead of the dropouts in MeV electrons that is the main contributor to the formation of
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leading edge of most spikes observed in the ratio curve.
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Figure S2-D compares the 90o telescope data (black) to the 0o telescope data (gray, timed
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by 20). Although the one-to-one correlation can be seen for the sudden increments in the
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two populations, electron levels measured by the 0o degree always recede much more
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quickly to the instrument back ground level of ~1 cnt/s. This is mainly due to the fact that
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in the outer belt the 0o telescope measures electrons well within the loss cone while the
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90o telescope mostly measures near and/or across the loss cone. Thus the higher flux
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levels for the larger pitch angles allow the 90o telescope to register more dynamic
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signatures. Indeed, much less dynamics are recorded by the 0o telescope of the E3 channel
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with even higher energy (not shown here). Due to these reasons, we chose to use POES
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measurements from the 90o telescope in this study, which provide more information to the
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predictive filters.
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3. Ruling out the Possibility of MeV Electron Contaminations on POES MEPED E2
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and E3 Channels
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The MagEIS instruments on board Van Allen Probes are believed to provide the cleanest
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electron observations on radiation belts that are often taken as the “gold standard”. Thus,
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using the level-3 pitch-angle resolved data from Van Allen Probes, we are able to derive
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the expected electron intensities at POES altitudes (called pseudo POES data here)
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following the methods described in Chen et al. [2014b]. As the example shown in Figure
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S3, since the dynamics shown in the pseudo data (Panel A) agree well with those in
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original POES E3 data (Panel B) particularly at L-shells between ~3.5 – 5.0, we believe
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MeV electrons have no significant effects on POES MEPED electron channels, and thus
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the cross-energy cross-pitch-angle discussed in the main text must be real. The difference
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in CR values between two panels are caused by errors from various sources, including
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such as mapping from the magnetic equator to low-altitudes, limited pitch-angle resolution
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for electrons near the loss-cone from Van Allen Probes’ near equatorial orbits, and no
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consideration of angular effects from MEPED’s wide opening angles. However, the
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difference in the absolute values in Panels A and B are not our concern for this study since
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we only need to compare how the pseudo data and real data vary over time. In addition,
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we also compare NOAA-15 data in two different MLT zones (predawn and afternoon) and
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see very different electron intensities (not shown here). Considering MeV electrons should
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have no MLT-dependence, the observed significant MLT-dependence in POES MEPED
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E2 and E3 channels provides another evidence supporting POES electron measurements
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used here should be reliable.
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4. Electron Radial Distributions and the roles of Magnetopause Shadowing and
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Radial Diffusion
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Here we evaluate the effects of Magnetopause shadowing and radial diffusion in the
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observed outer-belt electron dynamics. Figure S4-A plots the temporally evolving electron
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phase space density (PSD) radial distributions in the same period. In this plot electrons
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have the 1st adiabatic invariant µ=550MeV/G and the 2nd adiabatic K=0.03G0.5RE, which
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correspond to ~1MeV energy and ~45o equatorial pitch angle at L=4.6. The white symbols
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in Panel A mark the peak PSD positions in radial distributions, which are mostly at > ~5.5
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but sometimes move to as low as ~4.5. This is consistent from previous PSD studies by
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Chen et al. [2010] and Turner et al. [2012] that both show persistent PSD peaks exists at L
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between ~5-6 and negative PSD gradients at larger L-shells using THMEIS data. This
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suggests that 1 MeV electrons at L=4.6 are generally inside the PSD peak no matter
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during the loss or energization times. Therefore, the PSD peaks at larger L-shells and
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positive PSD radial gradients at L between 3.5 -5 do not favor outward radial diffusion,
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and thus the effects of magnetopause can be deemed unimportant for the dropouts of MeV
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electrons in this region; similarly, since persistent PSD peaks exists at L~5-6 instead of the
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outside of radial belt boundary, the role of magnetopause/plasma sheet can also be deemed
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insignificant for the energization of MeV electrons at L between 3.5-5.
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However, during MeV electron energization, it is possible that the inward radial diffusion
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from PSD peaks to smaller L-shells contributes to the cross-energy cross-pitch-angle
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coherence. Although quantifying the contribution of radial diffusion needs simulations
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from sophisticated models and thus is beyond the scope of this study, we may still do
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some quantitative evaluations. Using the empirical Kp-driven DLL from Brautigam and
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Albert [2000], we can estimate the time needed for a signature of new MeV electrons to
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propagate from beyond L=5 to L=3.5 through diffusion. Using the max Kp values during
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the period (Panel B), we can calculate the characteristic time ∫3.5 2𝐷 𝑑𝐿 to be >1.0 day
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with Kp =5 or >1.8 day with Kp=4. However, from the lag times for maximum CC for
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each L-shell in Figure 2, we know the lag-time difference for L-shells within 3.5 – 5 is
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<~10 h which is less than half of the diffusive time scales. In addition, we neither see the
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expected lag-time dependence due to inward radial diffusion—the time lag should
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increase significantly with decreasing L-shells—in the CC plots. Therefore, based upon
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above evaluations, we conclude that it is unlikely for the inward radial diffusion to
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dominate the time lags observed in the cross-energy cross-pitch-angle coherence.
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𝐿
𝐿𝐿
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References
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Brautigam, D.H. and J.M. Albert (2000), Radial diffusion analysis of outer radiation belt
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electrons during the October 9, 1990, magnetic storm, J. Geophy. Res., 105, A1, 291-
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Chen, Y. et al. (2014a), Global time-dependent chorus maps from low-Earth-orbit electron
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precipitation and Van Allen Probes data, Geophys. Res. Lett., 41,
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doi:10.1002/2013GL059181
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Chen, Y. et al. (2014b), REPAD: An empirical model of pitch-angle distributions for
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energetic electrons in the Earth’s outer radiation belt, J. Geophys. Res., 119,
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doi:10.1029/2013JA019431
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Chen, Y., G. Reeves, and R. Friedel (2010), On the role of transition region in controlling
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the outer radiation belt dynamics: A survey of in-situ observations, Fall AGU Meeting,
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SM33C-1920, San Francisco, CA, December 2010
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Turner, D.L., V. Angelopoulos, Y. Shprits, A. Kellerman, P. Cruce, and D. Larson (2012),
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Radiation distributions of equatorial phase space density for outer radiation belt
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electrons, Geo. Res. Lett., 39, L109101, doi: 10.1029/2012GL051722
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Figure S1 Validation of the chorus wave proxy method in a 3-month period. A)
Observed chorus wave amplitudes by Van Allen Probe-A, B) proxy chorus waves derived
from POES precipitating >30 keV electrons along Van Allen Probe-a trajectory, and C)
ratios between proxy values and observations. Colors from orange to dark gray indicate
good agreements. D) Dst (black) and AE (gray) indices. E, F, G) Validations using Van
Allen Probe-B data in the same format. All data are binned by 4.5 h and 0.2 in L.
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Figure S2 Count rates (CRs) for >100 keV electrons measured by NOAA-15 at L=4.6
within the same ~260 day period as in Figure 1. A) Ratios between CRs for
POES >100 keV electrons and RBSP 1MeV electron fluxes (replotted from Figure 1E). B)
Time series of >100 keV CRs (blue) compare to 1MeV electron fluxes (red). C) Dst
(black) and Kp (gray) indices. D) CRs for locally trapped (black) and precipitating
(gray) >100keV electrons measured at low altitude by NOAA-15. Here precipitating CRs
are timed by 20 to bring the curve close to that of locally trapped population.
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Figure S3 Testing possible MeV electron contaminations on POES MEPED E3
electron channel. A) Pseudo >300 keV electron observations at POES altitude, derived
from RBSP-a MagEIS pitch-angle resolved data, are sorted by L-shell and time. The time
period is the same as in Figure 1. B) Original POES E3 data in the same format. The two
black lines in both panels mark L=3.5 and 5.
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Figure S4 Electron radial PSD distributions vary with time (Panel A) and magnetic
activity (B, black for Dst and gray for Kp). Here electrons have the 1st adiabatic
invariant µ=550MeV/G and the 2nd adiabatic K=0.03G0.5RE, which correspond to ~1MeV
energy and ~45o equatorial pitch angle at L=4.6. White symbols in Panel A mark the
maximum PSD locations with L-shells between 3 – 6. Green vertical lines are identical to
those in Figure S2 indicating the spikes of in the ratios between >100 keV precipitating
and 1 MeV trapped electrons.
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