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 24259.87942407 -.00000011 00000-0 22058-3 0 9999
2 07530 101.9860 255.3972 0011849 271.6793 150.8665 12.53679480280649
| Epoch (UTC): | 15 September 2024 21:06:22 |
| Eccentricity: | 0.0011849 |
| inclination: | 101.9860° |
| perigee height: | 1440 km |
| apogee height: | 1458 km |
| right ascension of ascending node: | 255.3972° |
| argument of perigee: | 271.6793° |
| revolutions per day: | 12.53679480 |
| mean anomaly at epoch: | 150.8665° |
| orbit number at epoch: | 28064 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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