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 26107.74145272 +.00000000 +00000-0 +24540-4 0 00003
2 53807 53.2313 317.5853 0006033 9.2891 350.8224 15.37586020 06
| Epoch (UTC): | 17 April 2026 17:47:41 |
| Eccentricity: | 0.0006033 |
| inclination: | 53.2313° |
| perigee height: | 449 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 317.5853° |
| argument of perigee: | 9.2891° |
| revolutions per day: | 15.37586020 |
| mean anomaly at epoch: | 350.8224° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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