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 40024U 14033Q 23340.41123163 .00007050 00000-0 58757-3 0 9991
2 40024 98.0491 300.3896 0011416 68.0584 292.1850 14.98897703514188
| Epoch (UTC): | 06 December 2023 09:52:10 |
| Eccentricity: | 0.0011416 |
| inclination: | 98.0491° |
| perigee height: | 562 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 300.3896° |
| argument of perigee: | 68.0584° |
| revolutions per day: | 14.98897703 |
| mean anomaly at epoch: | 292.1850° |
| orbit number at epoch: | 51418 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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