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 56986U 23084BG 24279.79174533 .00085348 00000-0 24930-2 0 9992
2 56986 97.5483 41.1309 0009685 326.3333 33.7294 15.34932801 73106
| Epoch (UTC): | 05 October 2024 19:00:06 |
| Eccentricity: | 0.0009685 |
| inclination: | 97.5483° |
| perigee height: | 454 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 41.1309° |
| argument of perigee: | 326.3333° |
| revolutions per day: | 15.34932801 |
| mean anomaly at epoch: | 33.7294° |
| orbit number at epoch: | 7310 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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