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 38009U 11076C 23086.80016839 0.00001900 00000-0 29543-3 0 08
2 38009 97.8027 114.2407 0002205 80.1818 279.8826 14.73120109 09
| Epoch (UTC): | 27 March 2023 19:12:14 |
| Eccentricity: | 0.0002205 |
| inclination: | 97.8027° |
| perigee height: | 649 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 114.2407° |
| argument of perigee: | 80.1818° |
| revolutions per day: | 14.73120109 |
| mean anomaly at epoch: | 279.8826° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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