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 26044.74074866 +.00000000 +00000-0 +11804-3 0 00001
2 53807 53.2286 252.8802 0007483 142.6459 217.5067 15.36767856 03
| Epoch (UTC): | 13 February 2026 17:46:40 |
| Eccentricity: | 0.0007483 |
| inclination: | 53.2286° |
| perigee height: | 451 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 252.8802° |
| argument of perigee: | 142.6459° |
| revolutions per day: | 15.36767856 |
| mean anomaly at epoch: | 217.5067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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