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 39440U 13066AA 23091.79512181 .00005794 00000-0 75775-3 0 9994
2 39440 97.7645 43.1063 0074324 275.9726 83.3019 14.78867645502866
| Epoch (UTC): | 01 April 2023 19:04:58 |
| Eccentricity: | 0.0074324 |
| inclination: | 97.7645° |
| perigee height: | 581 km |
| apogee height: | 685 km |
| right ascension of ascending node: | 43.1063° |
| argument of perigee: | 275.9726° |
| revolutions per day: | 14.78867645 |
| mean anomaly at epoch: | 83.3019° |
| orbit number at epoch: | 50286 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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