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 00116U 61015A 25193.76865296 -.00000014 00000-0 47881-4 0 9998
2 00116 66.8107 1.3035 0072292 156.0293 204.4181 13.92246544249452
| Epoch (UTC): | 12 July 2025 18:26:51 |
| Eccentricity: | 0.0072292 |
| inclination: | 66.8107° |
| perigee height: | 868 km |
| apogee height: | 973 km |
| right ascension of ascending node: | 1.3035° |
| argument of perigee: | 156.0293° |
| revolutions per day: | 13.92246544 |
| mean anomaly at epoch: | 204.4181° |
| orbit number at epoch: | 24945 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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