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 65807U 26145.41523162 +.00000000 +00000-0 +31516-3 0 00000
2 65807 97.4481 8.1782 0002436 75.2000 284.9497 15.05656812 08
| Epoch (UTC): | 25 May 2026 09:57:56 |
| Eccentricity: | 0.0002436 |
| inclination: | 97.4481° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 8.1782° |
| argument of perigee: | 75.2000° |
| revolutions per day: | 15.05656812 |
| mean anomaly at epoch: | 284.9497° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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