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 23339.40987443 .00007157 00000-0 59663-3 0 9992
2 40024 98.0498 299.3553 0011513 70.8021 289.4446 14.98882297514033
| Epoch (UTC): | 05 December 2023 09:50:13 |
| Eccentricity: | 0.0011513 |
| inclination: | 98.0498° |
| perigee height: | 562 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 299.3553° |
| argument of perigee: | 70.8021° |
| revolutions per day: | 14.98882297 |
| mean anomaly at epoch: | 289.4446° |
| orbit number at epoch: | 51403 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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