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 43024U 17074C 24358.17333841 .00012411 00000-0 53298-3 0 9993
2 43024 97.4839 87.7980 0008417 2.4936 357.6340 15.22804462391171
| Epoch (UTC): | 23 December 2024 04:09:36 |
| Eccentricity: | 0.0008417 |
| inclination: | 97.4839° |
| perigee height: | 491 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 87.7980° |
| argument of perigee: | 2.4936° |
| revolutions per day: | 15.22804462 |
| mean anomaly at epoch: | 357.6340° |
| orbit number at epoch: | 39117 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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