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 26111.25147948 +.00000000 +00000-0 +69115-4 0 00003
2 53807 53.2305 301.1236 0006262 18.2471 341.8758 15.37601288 05
| Epoch (UTC): | 21 April 2026 06:02:07 |
| Eccentricity: | 0.0006262 |
| inclination: | 53.2305° |
| perigee height: | 449 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 301.1236° |
| argument of perigee: | 18.2471° |
| revolutions per day: | 15.37601288 |
| mean anomaly at epoch: | 341.8758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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