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 61323U 24140UL 24357.93846433 .00018588 00000-0 43764-2 0 9993
2 61323 88.8552 332.1834 0087888 320.6475 38.8367 14.51881302 16053
| Epoch (UTC): | 22 December 2024 22:31:23 |
| Eccentricity: | 0.0087888 |
| inclination: | 88.8552° |
| perigee height: | 657 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 332.1834° |
| argument of perigee: | 320.6475° |
| revolutions per day: | 14.51881302 |
| mean anomaly at epoch: | 38.8367° |
| orbit number at epoch: | 1605 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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