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 40012U 14033C 24262.41220302 .00007670 00000-0 96863-3 0 9993
2 40012 97.7136 61.1639 0051408 1.9915 358.1494 14.81222986551638
| Epoch (UTC): | 18 September 2024 09:53:34 |
| Eccentricity: | 0.0051408 |
| inclination: | 97.7136° |
| perigee height: | 589 km |
| apogee height: | 661 km |
| right ascension of ascending node: | 61.1639° |
| argument of perigee: | 1.9915° |
| revolutions per day: | 14.81222986 |
| mean anomaly at epoch: | 358.1494° |
| orbit number at epoch: | 55163 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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