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 24285U 26116.57490520 +.00000000 +00000-0 +33529-3 0 00007
2 24285 82.9473 70.9433 1737579 216.3814 130.5941 11.82592392 01
| Epoch (UTC): | 26 April 2026 13:47:51 |
| Eccentricity: | 0.1737579 |
| inclination: | 82.9473° |
| perigee height: | 346 km |
| apogee height: | 3174 km |
| right ascension of ascending node: | 70.9433° |
| argument of perigee: | 216.3814° |
| revolutions per day: | 11.82592392 |
| mean anomaly at epoch: | 130.5941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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