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 24259.87679662 .00033952 00000-0 23567-2 0 9994
2 39439 97.7183 222.9889 0039753 183.0888 177.0099 15.04833768584496
| Epoch (UTC): | 15 September 2024 21:02:35 |
| Eccentricity: | 0.0039753 |
| inclination: | 97.7183° |
| perigee height: | 524 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 222.9889° |
| argument of perigee: | 183.0888° |
| revolutions per day: | 15.04833768 |
| mean anomaly at epoch: | 177.0099° |
| orbit number at epoch: | 58449 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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