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 43666U 18083E 22280.40764625 .00016570 00000-0 66325-3 0 9997
2 43666 97.4147 307.9130 0010715 301.7567 172.7551 15.25090661218537
| Epoch (UTC): | 07 October 2022 09:47:00 |
| Eccentricity: | 0.0010715 |
| inclination: | 97.4147° |
| perigee height: | 483 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 307.9130° |
| argument of perigee: | 301.7567° |
| revolutions per day: | 15.25090661 |
| mean anomaly at epoch: | 172.7551° |
| orbit number at epoch: | 21853 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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