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 24256.54294274 -.00000012 00000-0 21616-3 0 9992
2 07530 101.9855 252.0277 0011870 278.2862 212.2683 12.53679338279989
| Epoch (UTC): | 12 September 2024 13:01:50 |
| Eccentricity: | 0.0011870 |
| inclination: | 101.9855° |
| perigee height: | 1440 km |
| apogee height: | 1458 km |
| right ascension of ascending node: | 252.0277° |
| argument of perigee: | 278.2862° |
| revolutions per day: | 12.53679338 |
| mean anomaly at epoch: | 212.2683° |
| orbit number at epoch: | 27998 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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