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 43017U 17073E 22229.35759277 .00004210 00000-0 31739-3 0 9998
2 43017 97.6665 121.0493 0247099 348.7491 10.8256 14.81807487256130
| Epoch (UTC): | 17 August 2022 08:34:56 |
| Eccentricity: | 0.0247099 |
| inclination: | 97.6665° |
| perigee height: | 450 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 121.0493° |
| argument of perigee: | 348.7491° |
| revolutions per day: | 14.81807487 |
| mean anomaly at epoch: | 10.8256° |
| orbit number at epoch: | 25613 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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