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 35122U 99025DLA 22226.53832221 .00000214 00000-0 14012-3 0 9996
2 35122 98.7906 259.5961 0026112 23.7483 336.4887 14.11999335466921
| Epoch (UTC): | 14 August 2022 12:55:11 |
| Eccentricity: | 0.0026112 |
| inclination: | 98.7906° |
| perigee height: | 833 km |
| apogee height: | 871 km |
| right ascension of ascending node: | 259.5961° |
| argument of perigee: | 23.7483° |
| revolutions per day: | 14.11999335 |
| mean anomaly at epoch: | 336.4887° |
| orbit number at epoch: | 46692 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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