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 39161U 13021C 22229.42363605 .00000758 00000-0 12553-3 0 9992
2 39161 97.9060 305.0728 0008244 222.0343 138.0233 14.73045455498449
| Epoch (UTC): | 17 August 2022 10:10:02 |
| Eccentricity: | 0.0008244 |
| inclination: | 97.9060° |
| perigee height: | 645 km |
| apogee height: | 657 km |
| right ascension of ascending node: | 305.0728° |
| argument of perigee: | 222.0343° |
| revolutions per day: | 14.73045455 |
| mean anomaly at epoch: | 138.0233° |
| orbit number at epoch: | 49844 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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