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 23160.43800297 .00005454 00000-0 50779-3 0 9995
2 40042 98.0078 108.9213 0011849 317.8480 42.1828 14.94669162486889
| Epoch (UTC): | 09 June 2023 10:30:43 |
| Eccentricity: | 0.0011849 |
| inclination: | 98.0078° |
| perigee height: | 575 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 108.9213° |
| argument of perigee: | 317.8480° |
| revolutions per day: | 14.94669162 |
| mean anomaly at epoch: | 42.1828° |
| orbit number at epoch: | 48688 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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