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 22177.18594085 .00000958 00000-0 15674-3 0 9994
2 39161 97.9076 254.1952 0010242 41.5902 318.6096 14.72969479490754
| Epoch (UTC): | 26 June 2022 04:27:45 |
| Eccentricity: | 0.0010242 |
| inclination: | 97.9076° |
| perigee height: | 644 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 254.1952° |
| argument of perigee: | 41.5902° |
| revolutions per day: | 14.72969479 |
| mean anomaly at epoch: | 318.6096° |
| orbit number at epoch: | 49075 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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