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 is defined by the following mean orbital elements,
1 40391U 15007B 22042.19918981 -.00027866 00000-0 00000+0 0 9995
2 40391 34.5090 11.5527 8233381 150.1422 25.2112 0.04100887 1310
| Epoch (UTC): | 11 February 2022 04:46:50 |
| Eccentricity: | 0.8233381 |
| inclination: | 34.5090° |
| perigee height: | 56373 km |
| apogee height: | 641279 km |
| right ascension of ascending node: | 11.5527° |
| argument of perigee: | 150.1422° |
| revolutions per day: | 0.04100887 |
| mean anomaly at epoch: | 25.2112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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