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 38758U 12048A 25162.91517831 0.00000000 00000-0 00000-0 0 00
2 38758 63.4262 73.5949 0278383 358.1891 1.8108 13.40972810 02
| Epoch (UTC): | 11 June 2025 21:57:51 |
| Eccentricity: | 0.0278383 |
| inclination: | 63.4262° |
| perigee height: | 897 km |
| apogee height: | 1314 km |
| right ascension of ascending node: | 73.5949° |
| argument of perigee: | 358.1891° |
| revolutions per day: | 13.40972810 |
| mean anomaly at epoch: | 1.8108° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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