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 52786U 26145.53766453 +.00000000 +00000-0 +24565-3 0 00003
2 52786 50.0016 307.3403 0023230 165.0764 195.0863 14.81292136 00
| Epoch (UTC): | 25 May 2026 12:54:14 |
| Eccentricity: | 0.0023230 |
| inclination: | 50.0016° |
| perigee height: | 609 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 307.3403° |
| argument of perigee: | 165.0764° |
| revolutions per day: | 14.81292136 |
| mean anomaly at epoch: | 195.0863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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