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 23439U 94085A 22342.40688371 -.00000039 00000-0 10000-3 0 9994
2 23439 64.8130 224.2558 0166870 242.9773 115.4032 11.27572988151109
| Epoch (UTC): | 08 December 2022 09:45:54 |
| Eccentricity: | 0.0166870 |
| inclination: | 64.8130° |
| perigee height: | 1882 km |
| apogee height: | 2162 km |
| right ascension of ascending node: | 224.2558° |
| argument of perigee: | 242.9773° |
| revolutions per day: | 11.27572988 |
| mean anomaly at epoch: | 115.4032° |
| orbit number at epoch: | 15110 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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