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 44475U 26052.48799524 +.00000000 +00000-0 +00000-0 0 00000
2 44475 0.0379 112.2141 0001206 224.9866 132.3686 1.00269882 08
| Epoch (UTC): | 21 February 2026 11:42:42 |
| Eccentricity: | 0.0001206 |
| inclination: | 0.0379° |
| perigee height: | 35782 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 112.2141° |
| argument of perigee: | 224.9866° |
| revolutions per day: | 1.00269882 |
| mean anomaly at epoch: | 132.3686° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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