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 22225.88761792 -.00000046 00000-0 -17869-5 0 9992
2 07530 101.9087 205.9478 0011908 293.2726 180.4781 12.53656290184661
| Epoch (UTC): | 13 August 2022 21:18:10 |
| Eccentricity: | 0.0011908 |
| inclination: | 101.9087° |
| perigee height: | 1440 km |
| apogee height: | 1458 km |
| right ascension of ascending node: | 205.9478° |
| argument of perigee: | 293.2726° |
| revolutions per day: | 12.53656290 |
| mean anomaly at epoch: | 180.4781° |
| orbit number at epoch: | 18466 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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