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 26131.91986666 +.00000000 +00000-0 +87472-4 0 00002
2 53807 53.2286 204.1731 0007368 67.5436 292.6349 15.37831088 03
| Epoch (UTC): | 11 May 2026 22:04:36 |
| Eccentricity: | 0.0007368 |
| inclination: | 53.2286° |
| perigee height: | 447 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 204.1731° |
| argument of perigee: | 67.5436° |
| revolutions per day: | 15.37831088 |
| mean anomaly at epoch: | 292.6349° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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