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 26045.97641432 +.00000000 +00000-0 +12714-3 0 00007
2 53807 53.2279 247.0909 0007545 147.8036 212.3430 15.36778278 03
| Epoch (UTC): | 14 February 2026 23:26:02 |
| Eccentricity: | 0.0007545 |
| inclination: | 53.2279° |
| perigee height: | 450 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 247.0909° |
| argument of perigee: | 147.8036° |
| revolutions per day: | 15.36778278 |
| mean anomaly at epoch: | 212.3430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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