View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 37841U 26031.73055766 +.00000000 +00000-0 +10305-3 0 00009
2 37841 19.9705 165.3954 0011717 142.0272 349.4444 14.11532942 08
| Epoch (UTC): | 31 January 2026 17:32:00 |
| Eccentricity: | 0.0011717 |
| inclination: | 19.9705° |
| perigee height: | 846 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 165.3954° |
| argument of perigee: | 142.0272° |
| revolutions per day: | 14.11532942 |
| mean anomaly at epoch: | 349.4444° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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