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 02050U 65082JL 24357.70283507 .00001963 00000-0 46641-3 0 9994
2 02050 32.2637 140.3727 0085412 338.6979 21.0122 14.50169697 79924
| Epoch (UTC): | 22 December 2024 16:52:04 |
| Eccentricity: | 0.0085412 |
| inclination: | 32.2637° |
| perigee height: | 664 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 140.3727° |
| argument of perigee: | 338.6979° |
| revolutions per day: | 14.50169697 |
| mean anomaly at epoch: | 21.0122° |
| orbit number at epoch: | 7992 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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