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 22179.54943344 .00001346 00000-0 14332-3 0 9998
2 40042 97.9713 118.2403 0014974 18.8713 341.3056 14.90570583435309
| Epoch (UTC): | 28 June 2022 13:11:11 |
| Eccentricity: | 0.0014974 |
| inclination: | 97.9713° |
| perigee height: | 586 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 118.2403° |
| argument of perigee: | 18.8713° |
| revolutions per day: | 14.90570583 |
| mean anomaly at epoch: | 341.3056° |
| orbit number at epoch: | 43530 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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