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 33401U 08051A 25206.97184344 -.00002141 00000-0 00000-0 0 9999
2 33401 46.2961 10.9471 7278850 50.1397 2.4308 0.10949703 5381
| Epoch (UTC): | 25 July 2025 23:19:27 |
| Eccentricity: | 0.7278850 |
| inclination: | 46.2961° |
| perigee height: | 43842 km |
| apogee height: | 312513 km |
| right ascension of ascending node: | 10.9471° |
| argument of perigee: | 50.1397° |
| revolutions per day: | 0.10949703 |
| mean anomaly at epoch: | 2.4308° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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