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 21942U 92021D 24357.56737339 .00005650 00000-0 51234-2 0 9999
2 21942 4.2914 105.5486 5945541 265.9081 28.3030 4.02490458376191
| Epoch (UTC): | 22 December 2024 13:37:01 |
| Eccentricity: | 0.5945541 |
| inclination: | 4.2914° |
| perigee height: | 390 km |
| apogee height: | 20241 km |
| right ascension of ascending node: | 105.5486° |
| argument of perigee: | 265.9081° |
| revolutions per day: | 4.02490458 |
| mean anomaly at epoch: | 28.3030° |
| orbit number at epoch: | 37619 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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