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 27432U 02024C 24281.42108156 .00000417 00000-0 23847-3 0 9999
2 27432 98.9633 324.2249 0051003 53.9305 317.4281 14.14381263155974
| Epoch (UTC): | 07 October 2024 10:06:21 |
| Eccentricity: | 0.0051003 |
| inclination: | 98.9633° |
| perigee height: | 807 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 324.2249° |
| argument of perigee: | 53.9305° |
| revolutions per day: | 14.14381263 |
| mean anomaly at epoch: | 317.4281° |
| orbit number at epoch: | 15597 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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