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 50831U 26145.36825560 +.00000000 +00000-0 +72503-4 0 00004
2 50831 53.2127 184.9649 0001021 86.0049 274.1060 15.08841143 06
| Epoch (UTC): | 25 May 2026 08:50:17 |
| Eccentricity: | 0.0001021 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 184.9649° |
| argument of perigee: | 86.0049° |
| revolutions per day: | 15.08841143 |
| mean anomaly at epoch: | 274.1060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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