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 39439U 13066Z 22177.44077690 .00002941 00000-0 34495-3 0 9994
2 39439 97.6365 150.9078 0063272 12.2112 348.0619 14.84277520463380
| Epoch (UTC): | 26 June 2022 10:34:43 |
| Eccentricity: | 0.0063272 |
| inclination: | 97.6365° |
| perigee height: | 571 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 150.9078° |
| argument of perigee: | 12.2112° |
| revolutions per day: | 14.84277520 |
| mean anomaly at epoch: | 348.0619° |
| orbit number at epoch: | 46338 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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