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 65869U 26145.58335647 +.00000000 +00000-0 -31617-3 0 00008
2 65869 53.1601 296.9351 0000829 82.0579 129.8060 15.34391426 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000829 |
| inclination: | 53.1601° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 296.9351° |
| argument of perigee: | 82.0579° |
| revolutions per day: | 15.34391426 |
| mean anomaly at epoch: | 129.8060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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