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 24955U 26022.47025553 +.00000000 +00000-0 +14622-3 0 00009
2 24955 82.9179 71.2840 0028178 275.3134 84.4811 13.81908546 07
| Epoch (UTC): | 22 January 2026 11:17:10 |
| Eccentricity: | 0.0028178 |
| inclination: | 82.9179° |
| perigee height: | 936 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 71.2840° |
| argument of perigee: | 275.3134° |
| revolutions per day: | 13.81908546 |
| mean anomaly at epoch: | 84.4811° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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