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 50830U 26145.42252398 +.00000000 +00000-0 -10180-3 0 00006
2 50830 53.2105 194.6547 0001286 76.1062 284.0073 15.08839028 07
| Epoch (UTC): | 25 May 2026 10:08:26 |
| Eccentricity: | 0.0001286 |
| inclination: | 53.2105° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 194.6547° |
| argument of perigee: | 76.1062° |
| revolutions per day: | 15.08839028 |
| mean anomaly at epoch: | 284.0073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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