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 22395U 92093CL 24357.81038170 .00014009 00000-0 39222-2 0 9997
2 22395 71.1410 241.7473 0065656 206.9330 220.5187 14.44898697642676
| Epoch (UTC): | 22 December 2024 19:26:56 |
| Eccentricity: | 0.0065656 |
| inclination: | 71.1410° |
| perigee height: | 695 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 241.7473° |
| argument of perigee: | 206.9330° |
| revolutions per day: | 14.44898697 |
| mean anomaly at epoch: | 220.5187° |
| orbit number at epoch: | 64267 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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