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 62509U 26145.55527975 +.00000000 +00000-0 +46436-3 0 00004
2 62509 42.9994 215.1780 0001413 273.2608 86.8082 15.27591669 05
| Epoch (UTC): | 25 May 2026 13:19:36 |
| Eccentricity: | 0.0001413 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 215.1780° |
| argument of perigee: | 273.2608° |
| revolutions per day: | 15.27591669 |
| mean anomaly at epoch: | 86.8082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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