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 24340.58146824 .00000194 00000-0 12352-3 0 9997
2 27432 98.9533 23.5508 0049343 245.0688 234.0375 14.14417822164331
| Epoch (UTC): | 05 December 2024 13:57:18 |
| Eccentricity: | 0.0049343 |
| inclination: | 98.9533° |
| perigee height: | 808 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 23.5508° |
| argument of perigee: | 245.0688° |
| revolutions per day: | 14.14417822 |
| mean anomaly at epoch: | 234.0375° |
| orbit number at epoch: | 16433 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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