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 26100.00629537 +.00000000 +00000-0 +12130-3 0 00007
2 53807 53.2313 353.8616 0005378 347.3047 12.7822 15.37553198 04
| Epoch (UTC): | 10 April 2026 00:09:03 |
| Eccentricity: | 0.0005378 |
| inclination: | 53.2313° |
| perigee height: | 450 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 353.8616° |
| argument of perigee: | 347.3047° |
| revolutions per day: | 15.37553198 |
| mean anomaly at epoch: | 12.7822° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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