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 24305U 96052B 22221.42214072 .00000065 00000-0 53336-4 0 9992
2 24305 82.9352 42.0763 0029400 209.4043 150.5459 13.73861891299303
| Epoch (UTC): | 09 August 2022 10:07:52 |
| Eccentricity: | 0.0029400 |
| inclination: | 82.9352° |
| perigee height: | 964 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 42.0763° |
| argument of perigee: | 209.4043° |
| revolutions per day: | 13.73861891 |
| mean anomaly at epoch: | 150.5459° |
| orbit number at epoch: | 29930 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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