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 40042U 14033AJ 24259.90792953 .00025775 00000-0 17727-2 0 9999
2 40042 98.0787 228.1402 0012771 171.7788 188.3649 15.05829282556475
| Epoch (UTC): | 15 September 2024 21:47:25 |
| Eccentricity: | 0.0012771 |
| inclination: | 98.0787° |
| perigee height: | 540 km |
| apogee height: | 558 km |
| right ascension of ascending node: | 228.1402° |
| argument of perigee: | 171.7788° |
| revolutions per day: | 15.05829282 |
| mean anomaly at epoch: | 188.3649° |
| orbit number at epoch: | 55647 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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