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 65879U 26145.40845431 +.00000000 +00000-0 +60134-3 0 00002
2 65879 53.1606 297.6792 0001307 75.0520 285.0627 15.34409333 05
| Epoch (UTC): | 25 May 2026 09:48:10 |
| Eccentricity: | 0.0001307 |
| inclination: | 53.1606° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 297.6792° |
| argument of perigee: | 75.0520° |
| revolutions per day: | 15.34409333 |
| mean anomaly at epoch: | 285.0627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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