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 23439U 94085A 22182.94206667 -.00000039 00000-0 10000-3 0 9999
2 23439 64.8150 122.1812 0168131 270.0743 88.0914 11.27572682133128
| Epoch (UTC): | 01 July 2022 22:36:34 |
| Eccentricity: | 0.0168131 |
| inclination: | 64.8150° |
| perigee height: | 1881 km |
| apogee height: | 2163 km |
| right ascension of ascending node: | 122.1812° |
| argument of perigee: | 270.0743° |
| revolutions per day: | 11.27572682 |
| mean anomaly at epoch: | 88.0914° |
| orbit number at epoch: | 13312 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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