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 27369U 02003C 22144.44342827 -.00000217 00000-0 00000-0 0 9990
2 27369 24.0396 277.5549 6860391 110.5608 331.5559 2.37187002175268
| Epoch (UTC): | 24 May 2022 10:38:32 |
| Eccentricity: | 0.6860391 |
| inclination: | 24.0396° |
| perigee height: | 1078 km |
| apogee height: | 33666 km |
| right ascension of ascending node: | 277.5549° |
| argument of perigee: | 110.5608° |
| revolutions per day: | 2.37187002 |
| mean anomaly at epoch: | 331.5559° |
| orbit number at epoch: | 17526 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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