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 38858U 12055B 25060.77336330 .00000028 00000-0 00000-0 0 9990
2 38858 55.5405 115.2181 0002939 278.1775 81.8829 1.64591902 5353
| Epoch (UTC): | 01 March 2025 18:33:38 |
| Eccentricity: | 0.0002939 |
| inclination: | 55.5405° |
| perigee height: | 23914 km |
| apogee height: | 23932 km |
| right ascension of ascending node: | 115.2181° |
| argument of perigee: | 278.1775° |
| revolutions per day: | 1.64591902 |
| mean anomaly at epoch: | 81.8829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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