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 65623U 26145.47421322 +.00000000 +00000-0 +76953-3 0 00001
2 65623 53.1590 309.2535 0001074 70.2427 289.8692 15.34411162 00
| Epoch (UTC): | 25 May 2026 11:22:52 |
| Eccentricity: | 0.0001074 |
| inclination: | 53.1590° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 309.2535° |
| argument of perigee: | 70.2427° |
| revolutions per day: | 15.34411162 |
| mean anomaly at epoch: | 289.8692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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