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 26042.00924657 +.00000000 +00000-0 +15319-3 0 00005
2 53807 53.2297 265.6735 0007865 136.0788 224.0843 15.36739128 04
| Epoch (UTC): | 11 February 2026 00:13:18 |
| Eccentricity: | 0.0007865 |
| inclination: | 53.2297° |
| perigee height: | 450 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 265.6735° |
| argument of perigee: | 136.0788° |
| revolutions per day: | 15.36739128 |
| mean anomaly at epoch: | 224.0843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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