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 62979U 26145.50593294 +.00000000 +00000-0 +56926-4 0 00003
2 62979 50.0061 317.1135 0001180 89.8144 270.2863 13.29318865 06
| Epoch (UTC): | 25 May 2026 12:08:32 |
| Eccentricity: | 0.0001180 |
| inclination: | 50.0061° |
| perigee height: | 1148 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 317.1135° |
| argument of perigee: | 89.8144° |
| revolutions per day: | 13.29318865 |
| mean anomaly at epoch: | 270.2863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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