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 25193.76237861 .00000063 00000-0 48257-4 0 9997
2 31114 98.3825 314.2596 0057870 271.9068 87.5482 14.20135724945660
| Epoch (UTC): | 12 July 2025 18:17:49 |
| Eccentricity: | 0.0057870 |
| inclination: | 98.3825° |
| perigee height: | 783 km |
| apogee height: | 866 km |
| right ascension of ascending node: | 314.2596° |
| argument of perigee: | 271.9068° |
| revolutions per day: | 14.20135724 |
| mean anomaly at epoch: | 87.5482° |
| orbit number at epoch: | 94566 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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