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 50817U 26145.48600988 +.00000000 +00000-0 +90527-4 0 00002
2 50817 53.2121 184.3678 0001336 77.1817 282.9325 15.08835270 08
| Epoch (UTC): | 25 May 2026 11:39:51 |
| Eccentricity: | 0.0001336 |
| inclination: | 53.2121° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 184.3678° |
| argument of perigee: | 77.1817° |
| revolutions per day: | 15.08835270 |
| mean anomaly at epoch: | 282.9325° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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