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 28522U 26088.03096189 +.00000000 +00000-0 -39447-4 0 00004
2 28522 82.9417 82.7232 0046795 100.0613 260.5836 13.90046571 04
| Epoch (UTC): | 29 March 2026 00:44:35 |
| Eccentricity: | 0.0046795 |
| inclination: | 82.9417° |
| perigee height: | 894 km |
| apogee height: | 963 km |
| right ascension of ascending node: | 82.7232° |
| argument of perigee: | 100.0613° |
| revolutions per day: | 13.90046571 |
| mean anomaly at epoch: | 260.5836° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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