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 19922U 26021.38169603 +.00000000 +00000-0 +69997-4 0 00007
2 19922 82.9564 256.9063 0037692 88.4878 272.0597 13.77490813 05
| Epoch (UTC): | 21 January 2026 09:09:38 |
| Eccentricity: | 0.0037692 |
| inclination: | 82.9564° |
| perigee height: | 945 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 256.9063° |
| argument of perigee: | 88.4878° |
| revolutions per day: | 13.77490813 |
| mean anomaly at epoch: | 272.0597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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