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 40014U 14033E 24337.87135105 .00009665 00000-0 63052-3 0 9994
2 40014 98.1036 28.2294 0031649 287.6356 72.1415 15.07693824571025
| Epoch (UTC): | 02 December 2024 20:54:44 |
| Eccentricity: | 0.0031649 |
| inclination: | 98.1036° |
| perigee height: | 521 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 28.2294° |
| argument of perigee: | 287.6356° |
| revolutions per day: | 15.07693824 |
| mean anomaly at epoch: | 72.1415° |
| orbit number at epoch: | 57102 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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