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 53807U 22111AL 23274.18084402 .00007794 00000-0 35030-3 0 9996
2 53807 53.2125 307.9947 0012699 25.9783 334.1850 15.22015554 58583
| Epoch (UTC): | 01 October 2023 04:20:24 |
| Eccentricity: | 0.0012699 |
| inclination: | 53.2125° |
| perigee height: | 491 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 307.9947° |
| argument of perigee: | 25.9783° |
| revolutions per day: | 15.22015554 |
| mean anomaly at epoch: | 334.1850° |
| orbit number at epoch: | 5858 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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