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 26017.94285497 +.00000000 +00000-0 +18648-3 0 00000
2 53807 53.2311 18.3608 0008293 73.9408 286.2509 15.36322558 01
| Epoch (UTC): | 17 January 2026 22:37:42 |
| Eccentricity: | 0.0008293 |
| inclination: | 53.2311° |
| perigee height: | 451 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 18.3608° |
| argument of perigee: | 73.9408° |
| revolutions per day: | 15.36322558 |
| mean anomaly at epoch: | 286.2509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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