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 23340.44927087 .00011257 00000-0 10400-2 0 9990
2 39439 97.7023 301.7184 0054777 65.6212 295.0712 14.93603680541909
| Epoch (UTC): | 06 December 2023 10:46:57 |
| Eccentricity: | 0.0054777 |
| inclination: | 97.7023° |
| perigee height: | 548 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 301.7184° |
| argument of perigee: | 65.6212° |
| revolutions per day: | 14.93603680 |
| mean anomaly at epoch: | 295.0712° |
| orbit number at epoch: | 54190 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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