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 53807U 26022.30135381 +.00000000 +00000-0 +20513-3 0 00006
2 53807 53.2315 357.9584 0008459 84.2070 275.9898 15.36423239 08
| Epoch (UTC): | 22 January 2026 07:13:56 |
| Eccentricity: | 0.0008459 |
| inclination: | 53.2315° |
| perigee height: | 451 km |
| apogee height: | 462 km |
| right ascension of ascending node: | 357.9584° |
| argument of perigee: | 84.2070° |
| revolutions per day: | 15.36423239 |
| mean anomaly at epoch: | 275.9898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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