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 40042U 14033AJ 22180.82489299 .00001425 00000-0 15137-3 0 9997
2 40042 97.9714 119.5274 0014897 14.9278 345.2376 14.90573866435492
| Epoch (UTC): | 29 June 2022 19:47:50 |
| Eccentricity: | 0.0014897 |
| inclination: | 97.9714° |
| perigee height: | 586 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 119.5274° |
| argument of perigee: | 14.9278° |
| revolutions per day: | 14.90573866 |
| mean anomaly at epoch: | 345.2376° |
| orbit number at epoch: | 43549 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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