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 39444U 13066AE 22176.47836654 .00001925 00000-0 23409-3 0 9999
2 39444 97.6238 150.0188 0056916 8.3091 351.9052 14.83461504462713
| Epoch (UTC): | 25 June 2022 11:28:50 |
| Eccentricity: | 0.0056916 |
| inclination: | 97.6238° |
| perigee height: | 578 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 150.0188° |
| argument of perigee: | 8.3091° |
| revolutions per day: | 14.83461504 |
| mean anomaly at epoch: | 351.9052° |
| orbit number at epoch: | 46271 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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