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 50201U 26145.38643758 +.00000000 +00000-0 +61421-3 0 00000
2 50201 53.1825 111.4149 0004381 50.4762 309.6660 16.09558466 05
| Epoch (UTC): | 25 May 2026 09:16:28 |
| Eccentricity: | 0.0004381 |
| inclination: | 53.1825° |
| perigee height: | 245 km |
| apogee height: | 251 km |
| right ascension of ascending node: | 111.4149° |
| argument of perigee: | 50.4762° |
| revolutions per day: | 16.09558466 |
| mean anomaly at epoch: | 309.6660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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