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 22175.89025422 .00002978 00000-0 34920-3 0 9990
2 39439 97.6364 149.4225 0063439 17.2906 343.0449 14.84266888463153
| Epoch (UTC): | 24 June 2022 21:21:57 |
| Eccentricity: | 0.0063439 |
| inclination: | 97.6364° |
| perigee height: | 571 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 149.4225° |
| argument of perigee: | 17.2906° |
| revolutions per day: | 14.84266888 |
| mean anomaly at epoch: | 343.0449° |
| orbit number at epoch: | 46315 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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