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 50198U 26145.58260698 +.00000000 +00000-0 +47669-4 0 00004
2 50198 53.2156 253.9342 0001210 90.2162 269.8969 15.08838457 07
| Epoch (UTC): | 25 May 2026 13:58:57 |
| Eccentricity: | 0.0001210 |
| inclination: | 53.2156° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 253.9342° |
| argument of perigee: | 90.2162° |
| revolutions per day: | 15.08838457 |
| mean anomaly at epoch: | 269.8969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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