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 50813U 26145.31859933 +.00000000 +00000-0 +95129-3 0 00008
2 50813 53.2029 122.6436 0002833 55.7805 304.3470 15.43322631 01
| Epoch (UTC): | 25 May 2026 07:38:46 |
| Eccentricity: | 0.0002833 |
| inclination: | 53.2029° |
| perigee height: | 434 km |
| apogee height: | 438 km |
| right ascension of ascending node: | 122.6436° |
| argument of perigee: | 55.7805° |
| revolutions per day: | 15.43322631 |
| mean anomaly at epoch: | 304.3470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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