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 37579U 99025EKC 22189.49766853 .00001139 00000-0 60811-3 0 9999
2 37579 99.2641 82.4072 0036800 310.0462 49.7483 14.15111685417505
| Epoch (UTC): | 08 July 2022 11:56:38 |
| Eccentricity: | 0.0036800 |
| inclination: | 99.2641° |
| perigee height: | 815 km |
| apogee height: | 868 km |
| right ascension of ascending node: | 82.4072° |
| argument of perigee: | 310.0462° |
| revolutions per day: | 14.15111685 |
| mean anomaly at epoch: | 49.7483° |
| orbit number at epoch: | 41750 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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