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 62975U 26145.58953928 +.00000000 +00000-0 +28889-4 0 00008
2 62975 50.0037 316.7996 0001168 99.2952 260.8053 13.29326602 07
| Epoch (UTC): | 25 May 2026 14:08:56 |
| Eccentricity: | 0.0001168 |
| inclination: | 50.0037° |
| perigee height: | 1148 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 316.7996° |
| argument of perigee: | 99.2952° |
| revolutions per day: | 13.29326602 |
| mean anomaly at epoch: | 260.8053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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