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 28158U 04004A 22224.99355027 -.00000236 00000-0 00000-0 0 9996
2 28158 10.1624 34.9518 0000453 160.1140 211.3936 1.00270284 18856
| Epoch (UTC): | 12 August 2022 23:50:42 |
| Eccentricity: | 0.0000453 |
| inclination: | 10.1624° |
| perigee height: | 35785 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 34.9518° |
| argument of perigee: | 160.1140° |
| revolutions per day: | 1.00270284 |
| mean anomaly at epoch: | 211.3936° |
| orbit number at epoch: | 1885 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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