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 50495U 26145.48521231 +.00000000 +00000-0 +90228-4 0 00005
2 50495 87.9161 339.9785 0001661 84.6461 275.4860 13.18687745 06
| Epoch (UTC): | 25 May 2026 11:38:42 |
| Eccentricity: | 0.0001661 |
| inclination: | 87.9161° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9785° |
| argument of perigee: | 84.6461° |
| revolutions per day: | 13.18687745 |
| mean anomaly at epoch: | 275.4860° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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