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 50163U 26145.66668980 +.00000000 +00000-0 +31327-2 0 00003
2 50163 53.2167 253.1582 0001543 65.3831 173.9839 15.16678504 09
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001543 |
| inclination: | 53.2167° |
| perigee height: | 515 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 253.1582° |
| argument of perigee: | 65.3831° |
| revolutions per day: | 15.16678504 |
| mean anomaly at epoch: | 173.9839° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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