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 26018.26812544 +.00000000 +00000-0 +19506-3 0 00009
2 53807 53.2315 16.8383 0008305 74.6475 285.5447 15.36327469 03
| Epoch (UTC): | 18 January 2026 06:26:06 |
| Eccentricity: | 0.0008305 |
| inclination: | 53.2315° |
| perigee height: | 451 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 16.8383° |
| argument of perigee: | 74.6475° |
| revolutions per day: | 15.36327469 |
| mean anomaly at epoch: | 285.5447° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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