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 50204U 26145.56884235 +.00000000 +00000-0 +86418-5 0 00005
2 50204 53.2151 254.0062 0001302 81.9599 278.1541 15.08845854 02
| Epoch (UTC): | 25 May 2026 13:39:07 |
| Eccentricity: | 0.0001302 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 254.0062° |
| argument of perigee: | 81.9599° |
| revolutions per day: | 15.08845854 |
| mean anomaly at epoch: | 278.1541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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