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 23341.47933640 .00005205 00000-0 43522-3 0 9991
2 40024 98.0492 301.4928 0011319 65.2410 294.9988 14.98909219514342
| Epoch (UTC): | 07 December 2023 11:30:14 |
| Eccentricity: | 0.0011319 |
| inclination: | 98.0492° |
| perigee height: | 562 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 301.4928° |
| argument of perigee: | 65.2410° |
| revolutions per day: | 14.98909219 |
| mean anomaly at epoch: | 294.9988° |
| orbit number at epoch: | 51434 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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