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 65642U 26144.82076590 +.00000000 +00000-0 +77924-3 0 00002
2 65642 53.1597 312.2857 0001190 99.9296 260.1841 15.34423982 01
| Epoch (UTC): | 24 May 2026 19:41:54 |
| Eccentricity: | 0.0001190 |
| inclination: | 53.1597° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 312.2857° |
| argument of perigee: | 99.9296° |
| revolutions per day: | 15.34423982 |
| mean anomaly at epoch: | 260.1841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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