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 43477U 18047B 22176.68032406 +.00001536 00000-0 +61728-4 0 08
2 43477 88.9868 37.3778 0014027 328.7256 124.2988 15.24810895227677
| Epoch (UTC): | 25 June 2022 16:19:39 |
| Eccentricity: | 0.0014027 |
| inclination: | 88.9868° |
| perigee height: | 482 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 37.3778° |
| argument of perigee: | 328.7256° |
| revolutions per day: | 15.24810895 |
| mean anomaly at epoch: | 124.2988° |
| orbit number at epoch: | 22767 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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