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 23150.89152489 .00007349 00000-0 75553-3 0 9992
2 39439 97.6785 116.9474 0055843 336.6136 23.2543 14.89459230513651
| Epoch (UTC): | 30 May 2023 21:23:47 |
| Eccentricity: | 0.0055843 |
| inclination: | 97.6785° |
| perigee height: | 560 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 116.9474° |
| argument of perigee: | 336.6136° |
| revolutions per day: | 14.89459230 |
| mean anomaly at epoch: | 23.2543° |
| orbit number at epoch: | 51365 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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