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 23339.84632685 .00012252 00000-0 11316-2 0 9992
2 39439 97.7019 301.1279 0054832 67.5003 293.2010 14.93590680541810
| Epoch (UTC): | 05 December 2023 20:18:42 |
| Eccentricity: | 0.0054832 |
| inclination: | 97.7019° |
| perigee height: | 548 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 301.1279° |
| argument of perigee: | 67.5003° |
| revolutions per day: | 14.93590680 |
| mean anomaly at epoch: | 293.2010° |
| orbit number at epoch: | 54181 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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