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 22181.90448163 -.00000050 00000-0 -24614-4 0 9990
2 07530 101.9044 161.8170 0012444 18.0823 36.9239 12.53655547179155
| Epoch (UTC): | 30 June 2022 21:42:27 |
| Eccentricity: | 0.0012444 |
| inclination: | 101.9044° |
| perigee height: | 1439 km |
| apogee height: | 1459 km |
| right ascension of ascending node: | 161.8170° |
| argument of perigee: | 18.0823° |
| revolutions per day: | 12.53655547 |
| mean anomaly at epoch: | 36.9239° |
| orbit number at epoch: | 17915 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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