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 08678U 75004F 24280.66428667 .00001332 00000-0 67067-3 0 9994
2 08678 97.6799 354.6695 0176417 148.9730 212.2009 14.09899807551411
| Epoch (UTC): | 06 October 2024 15:56:34 |
| Eccentricity: | 0.0176417 |
| inclination: | 97.6799° |
| perigee height: | 732 km |
| apogee height: | 987 km |
| right ascension of ascending node: | 354.6695° |
| argument of perigee: | 148.9730° |
| revolutions per day: | 14.09899807 |
| mean anomaly at epoch: | 212.2009° |
| orbit number at epoch: | 55141 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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