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CSSWE

In orbit NORAD 38761 MQNS-3492-8312-7376-9692 United States of America

—

Launch

6

Observations all time

Measure the directional differential flux of Solar Energetic Protons (SEPs) and Earth’s radiation belt electrons.

Mission description

Measure the directional differential flux of Solar Energetic Protons (SEPs) and Earth’s radiation belt electrons.

Mission information
Spacecraft name
CSSWE
Form factor
3U
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch time
Separation time
Satellite appearance

Credit: CSSWE CC BY-SA 3.0 source

Data for the last 30 days
Orbital parameters of the satellite
Perigee
396.75 km
Apogee
431.77 km
Inclination
64.7°
Period
92.9 min
Semi-major axis
6792.4 km
Velocity
7.68 km/s
Orbital elements
TLE source
Space-Track.org
TLE updated
2026-10-08 08:46:42 UTC
Two-line elements (TLE)
1 38761U 12048D   26280.74547411  .00032112  00000-0  55730-3 0  9993
2 38761 64.6611 70.5189 0025780 127.8010 232.5471 15.50344834133819
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-12 14:22:41 SITRO-AIS 38
NORAD 61786
CSSWE
NORAD 38761
4.864 12.49 1.2e-07
2026-10-14 09:50:03 GHGSAT-C6
NORAD 56204
CSSWE
NORAD 38761
3.147 14.75 1.9e-07
2026-10-16 10:55:03 STARLINK-4070
NORAD 52664
CSSWE
NORAD 38761
2.488 12.94 1.3e-05
2026-10-17 01:52:02 OBJECT K
NORAD 64885
CSSWE
NORAD 38761
2.895 14.04 2.6e-07
2026-10-17 11:46:20 GLOBAL-9
NORAD 47971
CSSWE
NORAD 38761
4.677 10.75 1.5e-07
2026-10-17 15:53:13 SKYSAT-C2
NORAD 41773
CSSWE
NORAD 38761
4.331 10.93 9.8e-08

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite