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 13992U 83031B 25196.91428809 .00000125 00000-0 50470-4 0 9991
2 13992 74.0536 352.3494 0005648 313.6079 46.4605 14.37388115212194
| Epoch (UTC): | 15 July 2025 21:56:34 |
| Eccentricity: | 0.0005648 |
| inclination: | 74.0536° |
| perigee height: | 763 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 352.3494° |
| argument of perigee: | 313.6079° |
| revolutions per day: | 14.37388115 |
| mean anomaly at epoch: | 46.4605° |
| orbit number at epoch: | 21219 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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