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 22176.55638156 -.00000039 00000-0 10000-3 0 9991
2 23439 64.8152 132.5086 0168149 271.1410 87.0254 11.27572667132409
| Epoch (UTC): | 25 June 2022 13:21:11 |
| Eccentricity: | 0.0168149 |
| inclination: | 64.8152° |
| perigee height: | 1881 km |
| apogee height: | 2163 km |
| right ascension of ascending node: | 132.5086° |
| argument of perigee: | 271.1410° |
| revolutions per day: | 11.27572667 |
| mean anomaly at epoch: | 87.0254° |
| orbit number at epoch: | 13240 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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