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 24260.82509164 .00013952 00000-0 12726-2 0 9999
2 39444 97.7271 218.2582 0045635 192.5425 167.4663 14.94407066583783
| Epoch (UTC): | 16 September 2024 19:48:07 |
| Eccentricity: | 0.0045635 |
| inclination: | 97.7271° |
| perigee height: | 552 km |
| apogee height: | 616 km |
| right ascension of ascending node: | 218.2582° |
| argument of perigee: | 192.5425° |
| revolutions per day: | 14.94407066 |
| mean anomaly at epoch: | 167.4663° |
| orbit number at epoch: | 58378 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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