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 39439U 13066Z 24260.34225475 .00028932 00000-0 20088-2 0 9994
2 39439 97.7183 223.4542 0039829 181.5625 178.5483 15.04857467585658
| Epoch (UTC): | 16 September 2024 08:12:50 |
| Eccentricity: | 0.0039829 |
| inclination: | 97.7183° |
| perigee height: | 524 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 223.4542° |
| argument of perigee: | 181.5625° |
| revolutions per day: | 15.04857467 |
| mean anomaly at epoch: | 178.5483° |
| orbit number at epoch: | 58565 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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