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 07530U 74089B 24357.87491228 -.00000022 00000-0 15194-3 0 9993
2 07530 101.9903 354.3697 0012400 84.2048 349.9067 12.53683995292686
| Epoch (UTC): | 22 December 2024 20:59:52 |
| Eccentricity: | 0.0012400 |
| inclination: | 101.9903° |
| perigee height: | 1439 km |
| apogee height: | 1459 km |
| right ascension of ascending node: | 354.3697° |
| argument of perigee: | 84.2048° |
| revolutions per day: | 12.53683995 |
| mean anomaly at epoch: | 349.9067° |
| orbit number at epoch: | 29268 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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