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 50189U 26145.34499735 +.00000000 +00000-0 +99886-3 0 00001
2 50189 53.2146 261.3453 0002839 26.1517 333.9621 15.15470873 02
| Epoch (UTC): | 25 May 2026 08:16:47 |
| Eccentricity: | 0.0002839 |
| inclination: | 53.2146° |
| perigee height: | 518 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 261.3453° |
| argument of perigee: | 26.1517° |
| revolutions per day: | 15.15470873 |
| mean anomaly at epoch: | 333.9621° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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