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 50832U 26145.42349199 +.00000000 +00000-0 -91323-5 0 00004
2 50832 53.2104 194.6984 0001253 72.9965 287.1165 15.08834825 09
| Epoch (UTC): | 25 May 2026 10:09:49 |
| Eccentricity: | 0.0001253 |
| inclination: | 53.2104° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 194.6984° |
| argument of perigee: | 72.9965° |
| revolutions per day: | 15.08834825 |
| mean anomaly at epoch: | 287.1165° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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