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 26121.71607282 +.00000000 +00000-0 +16808-3 0 00007
2 53807 53.2291 252.0406 0006980 44.5219 315.6345 15.37722579 09
| Epoch (UTC): | 01 May 2026 17:11:08 |
| Eccentricity: | 0.0006980 |
| inclination: | 53.2291° |
| perigee height: | 448 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 252.0406° |
| argument of perigee: | 44.5219° |
| revolutions per day: | 15.37722579 |
| mean anomaly at epoch: | 315.6345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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