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 06323U 72104A 24357.48040270 .00000348 00000-0 12525-3 0 9997
2 06323 74.0810 13.6379 0016621 120.1959 240.0843 14.37200454721188
| Epoch (UTC): | 22 December 2024 11:31:46 |
| Eccentricity: | 0.0016621 |
| inclination: | 74.0810° |
| perigee height: | 756 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 13.6379° |
| argument of perigee: | 120.1959° |
| revolutions per day: | 14.37200454 |
| mean anomaly at epoch: | 240.0843° |
| orbit number at epoch: | 72118 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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