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 23147.86840295 .00006537 00000-0 67332-3 0 9998
2 39439 97.6793 114.0131 0056131 346.8900 13.0856 14.89415602513202
| Epoch (UTC): | 27 May 2023 20:50:30 |
| Eccentricity: | 0.0056131 |
| inclination: | 97.6793° |
| perigee height: | 560 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 114.0131° |
| argument of perigee: | 346.8900° |
| revolutions per day: | 14.89415602 |
| mean anomaly at epoch: | 13.0856° |
| orbit number at epoch: | 51320 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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