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 22237U 92080B 24278.75982047 .00001863 00000-0 24501-3 0 9993
2 22237 82.5128 156.1915 0020601 119.7880 240.5386 14.79578454717383
| Epoch (UTC): | 04 October 2024 18:14:08 |
| Eccentricity: | 0.0020601 |
| inclination: | 82.5128° |
| perigee height: | 616 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 156.1915° |
| argument of perigee: | 119.7880° |
| revolutions per day: | 14.79578454 |
| mean anomaly at epoch: | 240.5386° |
| orbit number at epoch: | 71738 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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