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 6324U 72104B 23147.41187810 .00000256 00000-0 82825-4 0 9998
2 6324 74.0791 43.2114 0009125 336.8355 23.2390 14.43929568648727
| Epoch (UTC): | 27 May 2023 09:53:06 |
| Eccentricity: | 0.0009125 |
| inclination: | 74.0791° |
| perigee height: | 739 km |
| apogee height: | 752 km |
| right ascension of ascending node: | 43.2114° |
| argument of perigee: | 336.8355° |
| revolutions per day: | 14.43929568 |
| mean anomaly at epoch: | 23.2390° |
| orbit number at epoch: | 64872 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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