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 14781U 84021B 22182.54654478 .00000308 00000-0 43380-4 0 9997
2 14781 97.6174 169.3384 0006808 277.3571 82.6870 14.83695805 63138
| Epoch (UTC): | 01 July 2022 13:07:01 |
| Eccentricity: | 0.0006808 |
| inclination: | 97.6174° |
| perigee height: | 613 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 169.3384° |
| argument of perigee: | 277.3571° |
| revolutions per day: | 14.83695805 |
| mean anomaly at epoch: | 82.6870° |
| orbit number at epoch: | 6313 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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