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 42340U 00055QG 24251.56363534 .00031500 00000-0 13253-1 0 9996
2 42340 99.0323 12.9508 0035965 347.6212 12.4079 14.25293134438887
| Epoch (UTC): | 07 September 2024 13:31:38 |
| Eccentricity: | 0.0035965 |
| inclination: | 99.0323° |
| perigee height: | 781 km |
| apogee height: | 833 km |
| right ascension of ascending node: | 12.9508° |
| argument of perigee: | 347.6212° |
| revolutions per day: | 14.25293134 |
| mean anomaly at epoch: | 12.4079° |
| orbit number at epoch: | 43888 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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