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 43152U 18007A 24358.18246753 .00015760 00000-0 68389-3 0 9995
2 43152 97.4082 2.2383 0001528 93.5344 266.6067 15.22419854385100
| Epoch (UTC): | 23 December 2024 04:22:45 |
| Eccentricity: | 0.0001528 |
| inclination: | 97.4082° |
| perigee height: | 497 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 2.2383° |
| argument of perigee: | 93.5344° |
| revolutions per day: | 15.22419854 |
| mean anomaly at epoch: | 266.6067° |
| orbit number at epoch: | 38510 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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