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 22180.44659032 .00000909 00000-0 12922-3 0 9999
2 39440 97.7266 137.4993 0080353 92.4566 268.5847 14.77032742462050
| Epoch (UTC): | 29 June 2022 10:43:05 |
| Eccentricity: | 0.0080353 |
| inclination: | 97.7266° |
| perigee height: | 582 km |
| apogee height: | 695 km |
| right ascension of ascending node: | 137.4993° |
| argument of perigee: | 92.4566° |
| revolutions per day: | 14.77032742 |
| mean anomaly at epoch: | 268.5847° |
| orbit number at epoch: | 46205 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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