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 04611U 70025P 23344.77326785 .00000646 00000-0 42434-3 0 9993
2 04611 99.7966 259.3413 0126897 72.0296 289.4652 14.02083775726778
| Epoch (UTC): | 10 December 2023 18:33:30 |
| Eccentricity: | 0.0126897 |
| inclination: | 99.7966° |
| perigee height: | 794 km |
| apogee height: | 979 km |
| right ascension of ascending node: | 259.3413° |
| argument of perigee: | 72.0296° |
| revolutions per day: | 14.02083775 |
| mean anomaly at epoch: | 289.4652° |
| orbit number at epoch: | 72677 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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