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 40057U 14034E 24262.86193822 .00006915 00000-0 76448-3 0 9996
2 40057 98.3285 122.5962 0008279 189.7141 170.3915 14.87714341551622
| Epoch (UTC): | 18 September 2024 20:41:11 |
| Eccentricity: | 0.0008279 |
| inclination: | 98.3285° |
| perigee height: | 599 km |
| apogee height: | 611 km |
| right ascension of ascending node: | 122.5962° |
| argument of perigee: | 189.7141° |
| revolutions per day: | 14.87714341 |
| mean anomaly at epoch: | 170.3915° |
| orbit number at epoch: | 55162 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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