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 data is extracted from the following two-line orbital elements,
1 38858U 12055B 25042.54689446 -.00000019 00000-0 00000+0 0 9994
2 38858 55.5308 115.6831 0000761 269.5264 90.5214 1.64591971 76572
| Epoch (UTC): | 11 February 2025 13:07:31 |
| Eccentricity: | 0.0000761 |
| inclination: | 55.5308° |
| perigee height: | 23921 km |
| apogee height: | 23925 km |
| right ascension of ascending node: | 115.6831° |
| argument of perigee: | 269.5264° |
| revolutions per day: | 1.64591971 |
| mean anomaly at epoch: | 90.5214° |
| orbit number at epoch: | 7657 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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