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 39440U 13066AA 24340.40715823 .00010054 00000-0 10872-2 0 9999
2 39440 97.8314 280.8918 0067966 73.4554 287.4113 14.86782551593743
| Epoch (UTC): | 05 December 2024 09:46:18 |
| Eccentricity: | 0.0067966 |
| inclination: | 97.8314° |
| perigee height: | 560 km |
| apogee height: | 655 km |
| right ascension of ascending node: | 280.8918° |
| argument of perigee: | 73.4554° |
| revolutions per day: | 14.86782551 |
| mean anomaly at epoch: | 287.4113° |
| orbit number at epoch: | 59374 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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