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 00047U 60007C 24262.57398217 .00001911 00000-0 42932-3 0 9997
2 00047 66.6668 316.0820 0229885 246.1945 111.4909 14.43875430358848
| Epoch (UTC): | 18 September 2024 13:46:32 |
| Eccentricity: | 0.0229885 |
| inclination: | 66.6668° |
| perigee height: | 582 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 316.0820° |
| argument of perigee: | 246.1945° |
| revolutions per day: | 14.43875430 |
| mean anomaly at epoch: | 111.4909° |
| orbit number at epoch: | 35884 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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