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 39440U 13066AA 22176.44964152 .00001223 00000-0 17141-3 0 9994
2 39440 97.7263 133.6702 0080269 105.1594 255.8512 14.77024021461465
| Epoch (UTC): | 25 June 2022 10:47:29 |
| Eccentricity: | 0.0080269 |
| inclination: | 97.7263° |
| perigee height: | 582 km |
| apogee height: | 695 km |
| right ascension of ascending node: | 133.6702° |
| argument of perigee: | 105.1594° |
| revolutions per day: | 14.77024021 |
| mean anomaly at epoch: | 255.8512° |
| orbit number at epoch: | 46146 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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