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 46265U 20059A 22229.06591863 .00000828 00000-0 11060-3 0 9993
2 46265 97.8879 53.9585 0001460 82.8444 277.2923 14.82162909106101
| Epoch (UTC): | 17 August 2022 01:34:55 |
| Eccentricity: | 0.0001460 |
| inclination: | 97.8879° |
| perigee height: | 621 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 53.9585° |
| argument of perigee: | 82.8444° |
| revolutions per day: | 14.82162909 |
| mean anomaly at epoch: | 277.2923° |
| orbit number at epoch: | 10610 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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