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 40907U 15049J 22180.87144771 .00004629 00000-0 21869-3 0 9991
2 40907 97.4907 184.1758 0011670 318.3840 159.1878 15.19862392374856
| Epoch (UTC): | 29 June 2022 20:54:53 |
| Eccentricity: | 0.0011670 |
| inclination: | 97.4907° |
| perigee height: | 498 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 184.1758° |
| argument of perigee: | 318.3840° |
| revolutions per day: | 15.19862392 |
| mean anomaly at epoch: | 159.1878° |
| orbit number at epoch: | 37485 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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