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 26046.88689772 +.00000000 +00000-0 +17534-3 0 00002
2 53807 53.2280 242.8263 0007402 149.8746 210.2686 15.36791468 09
| Epoch (UTC): | 15 February 2026 21:17:07 |
| Eccentricity: | 0.0007402 |
| inclination: | 53.2280° |
| perigee height: | 451 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 242.8263° |
| argument of perigee: | 149.8746° |
| revolutions per day: | 15.36791468 |
| mean anomaly at epoch: | 210.2686° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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