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 44854U 19089C 25342.89580904 .10801921 36355-5 10723-2 0 9995
2 44854 36.9163 249.0625 0006835 253.5286 106.4749 16.36980482331539
| Epoch (UTC): | 08 December 2025 21:29:57 |
| Eccentricity: | 0.0006835 |
| inclination: | 36.9163° |
| perigee height: | 169 km |
| apogee height: | 178 km |
| right ascension of ascending node: | 249.0625° |
| argument of perigee: | 253.5286° |
| revolutions per day: | 16.36980482 |
| mean anomaly at epoch: | 106.4749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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