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 09619U 75004FU 24357.79309742 .00004715 00000-0 12386-2 0 9992
2 09619 97.4003 38.9991 0102551 241.8768 117.2033 14.46432667593039
| Epoch (UTC): | 22 December 2024 19:02:03 |
| Eccentricity: | 0.0102551 |
| inclination: | 97.4003° |
| perigee height: | 664 km |
| apogee height: | 810 km |
| right ascension of ascending node: | 38.9991° |
| argument of perigee: | 241.8768° |
| revolutions per day: | 14.46432667 |
| mean anomaly at epoch: | 117.2033° |
| orbit number at epoch: | 59303 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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