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 39444U 13066AE 24259.61983314 .00015337 00000-0 13993-2 0 9993
2 39444 97.7265 217.0718 0045548 196.7810 163.1906 14.94376715583601
| Epoch (UTC): | 15 September 2024 14:52:33 |
| Eccentricity: | 0.0045548 |
| inclination: | 97.7265° |
| perigee height: | 552 km |
| apogee height: | 616 km |
| right ascension of ascending node: | 217.0718° |
| argument of perigee: | 196.7810° |
| revolutions per day: | 14.94376715 |
| mean anomaly at epoch: | 163.1906° |
| orbit number at epoch: | 58360 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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