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 24287.50968038 -.00000003 00000-0 26987-3 0 9994
2 07530 101.9881 283.3031 0011932 217.6311 294.3867 12.53680877283865
| Epoch (UTC): | 13 October 2024 12:13:56 |
| Eccentricity: | 0.0011932 |
| inclination: | 101.9881° |
| perigee height: | 1440 km |
| apogee height: | 1458 km |
| right ascension of ascending node: | 283.3031° |
| argument of perigee: | 217.6311° |
| revolutions per day: | 12.53680877 |
| mean anomaly at epoch: | 294.3867° |
| orbit number at epoch: | 28386 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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