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 65714U 25214C 25341.27396551 .00005671 00000-0 65050-3 0 9998
2 65714 49.9829 117.8483 0013102 210.3142 149.7041 14.87026398 11015
| Epoch (UTC): | 07 December 2025 06:34:30 |
| Eccentricity: | 0.0013102 |
| inclination: | 49.9829° |
| perigee height: | 598 km |
| apogee height: | 616 km |
| right ascension of ascending node: | 117.8483° |
| argument of perigee: | 210.3142° |
| revolutions per day: | 14.87026398 |
| mean anomaly at epoch: | 149.7041° |
| orbit number at epoch: | 1101 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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