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 31114U 07010B 25318.81935330 .00000331 00000-0 17176-3 0 9991
2 31114 98.3963 72.8774 0057913 268.1439 91.3105 14.20193135963414
| Epoch (UTC): | 14 November 2025 19:39:52 |
| Eccentricity: | 0.0057913 |
| inclination: | 98.3963° |
| perigee height: | 783 km |
| apogee height: | 866 km |
| right ascension of ascending node: | 72.8774° |
| argument of perigee: | 268.1439° |
| revolutions per day: | 14.20193135 |
| mean anomaly at epoch: | 91.3105° |
| orbit number at epoch: | 96341 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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