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 04320U 70008A 22228.41074231 -.00000030 00000-0 90721-4 0 9999
2 04320 101.5850 290.5381 0028670 158.5636 212.5330 12.52072134598540
| Epoch (UTC): | 16 August 2022 09:51:28 |
| Eccentricity: | 0.0028670 |
| inclination: | 101.5850° |
| perigee height: | 1433 km |
| apogee height: | 1478 km |
| right ascension of ascending node: | 290.5381° |
| argument of perigee: | 158.5636° |
| revolutions per day: | 12.52072134 |
| mean anomaly at epoch: | 212.5330° |
| orbit number at epoch: | 59854 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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