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 23335.87165868 .00014425 00000-0 11981-2 0 9994
2 40024 98.0509 295.7018 0011814 80.0904 280.1651 14.98811748514027
| Epoch (UTC): | 01 December 2023 20:55:11 |
| Eccentricity: | 0.0011814 |
| inclination: | 98.0509° |
| perigee height: | 562 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 295.7018° |
| argument of perigee: | 80.0904° |
| revolutions per day: | 14.98811748 |
| mean anomaly at epoch: | 280.1651° |
| orbit number at epoch: | 51402 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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