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 40263U 14059C 24281.18775393 .00055176 00000-0 88609-2 0 9991
2 40263 98.1989 9.7568 0081300 116.4765 244.4808 14.69151054531632
| Epoch (UTC): | 07 October 2024 04:30:21 |
| Eccentricity: | 0.0081300 |
| inclination: | 98.1989° |
| perigee height: | 606 km |
| apogee height: | 721 km |
| right ascension of ascending node: | 9.7568° |
| argument of perigee: | 116.4765° |
| revolutions per day: | 14.69151054 |
| mean anomaly at epoch: | 244.4808° |
| orbit number at epoch: | 53163 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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