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 24773U 26020.97710453 +.00000000 +00000-0 +24747-3 0 00009
2 24773 82.9193 205.8285 0023789 205.4240 266.2363 13.73960929 00
| Epoch (UTC): | 20 January 2026 23:27:01 |
| Eccentricity: | 0.0023789 |
| inclination: | 82.9193° |
| perigee height: | 968 km |
| apogee height: | 1003 km |
| right ascension of ascending node: | 205.8285° |
| argument of perigee: | 205.4240° |
| revolutions per day: | 13.73960929 |
| mean anomaly at epoch: | 266.2363° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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