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 10457U 77106A 24277.89109530 .00000289 00000-0 44515-3 0 9996
2 10457 89.6445 94.1037 0025724 12.1470 115.5799 13.48842894309037
| Epoch (UTC): | 03 October 2024 21:23:10 |
| Eccentricity: | 0.0025724 |
| inclination: | 89.6445° |
| perigee height: | 1057 km |
| apogee height: | 1095 km |
| right ascension of ascending node: | 94.1037° |
| argument of perigee: | 12.1470° |
| revolutions per day: | 13.48842894 |
| mean anomaly at epoch: | 115.5799° |
| orbit number at epoch: | 30903 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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