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 51950U 26145.64410884 +.00000000 +00000-0 +10434-3 0 00001
2 51950 63.4633 12.3891 0157996 348.6810 11.0684 13.56283115 03
| Epoch (UTC): | 25 May 2026 15:27:31 |
| Eccentricity: | 0.0157996 |
| inclination: | 63.4633° |
| perigee height: | 932 km |
| apogee height: | 1167 km |
| right ascension of ascending node: | 12.3891° |
| argument of perigee: | 348.6810° |
| revolutions per day: | 13.56283115 |
| mean anomaly at epoch: | 11.0684° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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