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 22175.83993459 .00001243 00000-0 17413-3 0 9992
2 39440 97.7262 133.0861 0080245 107.0983 253.9036 14.77022281461377
| Epoch (UTC): | 24 June 2022 20:09:30 |
| Eccentricity: | 0.0080245 |
| inclination: | 97.7262° |
| perigee height: | 582 km |
| apogee height: | 695 km |
| right ascension of ascending node: | 133.0861° |
| argument of perigee: | 107.0983° |
| revolutions per day: | 14.77022281 |
| mean anomaly at epoch: | 253.9036° |
| orbit number at epoch: | 46137 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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