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 24357.81852175 .00009967 00000-0 10365-2 0 9994
2 40057 98.3150 222.3637 0007277 251.2365 108.8062 14.90075028565755
| Epoch (UTC): | 22 December 2024 19:38:40 |
| Eccentricity: | 0.0007277 |
| inclination: | 98.3150° |
| perigee height: | 592 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 222.3637° |
| argument of perigee: | 251.2365° |
| revolutions per day: | 14.90075028 |
| mean anomaly at epoch: | 108.8062° |
| orbit number at epoch: | 56575 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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