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 50572U 26145.64123233 +.00000000 +00000-0 +11759-3 0 00000
2 50572 88.9704 325.9383 0009566 141.2783 218.9164 15.46150872 02
| Epoch (UTC): | 25 May 2026 15:23:22 |
| Eccentricity: | 0.0009566 |
| inclination: | 88.9704° |
| perigee height: | 421 km |
| apogee height: | 435 km |
| right ascension of ascending node: | 325.9383° |
| argument of perigee: | 141.2783° |
| revolutions per day: | 15.46150872 |
| mean anomaly at epoch: | 218.9164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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