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 22179.90980939 -.00000048 00000-0 -14039-4 0 9996
2 07530 101.9042 159.8160 0012469 21.8094 34.7430 12.53655581178907
| Epoch (UTC): | 28 June 2022 21:50:07 |
| Eccentricity: | 0.0012469 |
| inclination: | 101.9042° |
| perigee height: | 1439 km |
| apogee height: | 1459 km |
| right ascension of ascending node: | 159.8160° |
| argument of perigee: | 21.8094° |
| revolutions per day: | 12.53655581 |
| mean anomaly at epoch: | 34.7430° |
| orbit number at epoch: | 17890 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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