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 06393U 73015B 25196.89065795 .00000029 00000-0 10251-4 0 9993
2 06393 81.2576 343.5755 0057273 266.2894 93.1724 14.05377141681098
| Epoch (UTC): | 15 July 2025 21:22:32 |
| Eccentricity: | 0.0057273 |
| inclination: | 81.2576° |
| perigee height: | 833 km |
| apogee height: | 917 km |
| right ascension of ascending node: | 343.5755° |
| argument of perigee: | 266.2894° |
| revolutions per day: | 14.05377141 |
| mean anomaly at epoch: | 93.1724° |
| orbit number at epoch: | 68109 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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