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 40042U 14033AJ 22176.39433895 .00002106 00000-0 22085-3 0 9992
2 40042 97.9709 115.0559 0015276 28.9250 331.2811 14.90559491434834
| Epoch (UTC): | 25 June 2022 09:27:50 |
| Eccentricity: | 0.0015276 |
| inclination: | 97.9709° |
| perigee height: | 585 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 115.0559° |
| argument of perigee: | 28.9250° |
| revolutions per day: | 14.90559491 |
| mean anomaly at epoch: | 331.2811° |
| orbit number at epoch: | 43483 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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