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 50199U 26145.56421306 +.00000000 +00000-0 +37577-3 0 00004
2 50199 53.2127 254.0154 0001252 73.7290 286.3840 15.08861911 06
| Epoch (UTC): | 25 May 2026 13:32:28 |
| Eccentricity: | 0.0001252 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 254.0154° |
| argument of perigee: | 73.7290° |
| revolutions per day: | 15.08861911 |
| mean anomaly at epoch: | 286.3840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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