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 58848U 23174DH 24281.15540787 .00011495 00000-0 70726-3 0 9999
2 58848 97.4231 348.8158 0011615 355.8646 4.2486 15.10120973 50423
| Epoch (UTC): | 07 October 2024 03:43:47 |
| Eccentricity: | 0.0011615 |
| inclination: | 97.4231° |
| perigee height: | 528 km |
| apogee height: | 544 km |
| right ascension of ascending node: | 348.8158° |
| argument of perigee: | 355.8646° |
| revolutions per day: | 15.10120973 |
| mean anomaly at epoch: | 4.2486° |
| orbit number at epoch: | 5042 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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