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 14466U 70025NS 22222.23677776 .00001972 00000-0 70590-3 0 9993
2 14466 99.9646 147.8629 0068420 10.1649 350.0897 14.34104049109152
| Epoch (UTC): | 10 August 2022 05:40:57 |
| Eccentricity: | 0.0068420 |
| inclination: | 99.9646° |
| perigee height: | 729 km |
| apogee height: | 827 km |
| right ascension of ascending node: | 147.8629° |
| argument of perigee: | 10.1649° |
| revolutions per day: | 14.34104049 |
| mean anomaly at epoch: | 350.0897° |
| orbit number at epoch: | 10915 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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