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 50815U 26145.48969340 +.00000000 +00000-0 -18247-4 0 00000
2 50815 53.2124 184.3498 0001234 77.6184 282.4946 15.08834077 06
| Epoch (UTC): | 25 May 2026 11:45:09 |
| Eccentricity: | 0.0001234 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 184.3498° |
| argument of perigee: | 77.6184° |
| revolutions per day: | 15.08834077 |
| mean anomaly at epoch: | 282.4946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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