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 62899U 26145.63017863 +.00000000 +00000-0 +56331-3 0 00000
2 62899 42.9991 250.7869 0001558 276.6688 83.3986 15.27592036 06
| Epoch (UTC): | 25 May 2026 15:07:27 |
| Eccentricity: | 0.0001558 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 250.7869° |
| argument of perigee: | 276.6688° |
| revolutions per day: | 15.27592036 |
| mean anomaly at epoch: | 83.3986° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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