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 00051U 60009C 24255.33122060 -.00000008 00000-0 75740-3 0 9991
2 00051 47.2105 241.6274 0105584 81.4664 279.8073 12.18333486852678
| Epoch (UTC): | 11 September 2024 07:56:57 |
| Eccentricity: | 0.0105584 |
| inclination: | 47.2105° |
| perigee height: | 1515 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 241.6274° |
| argument of perigee: | 81.4664° |
| revolutions per day: | 12.18333486 |
| mean anomaly at epoch: | 279.8073° |
| orbit number at epoch: | 85267 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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