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 23266.42028722 .00005398 00000-0 68392-3 0 9998
2 39440 97.7786 212.0418 0076174 68.0267 292.9018 14.80108315528689
| Epoch (UTC): | 23 September 2023 10:05:12 |
| Eccentricity: | 0.0076174 |
| inclination: | 97.7786° |
| perigee height: | 575 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 212.0418° |
| argument of perigee: | 68.0267° |
| revolutions per day: | 14.80108315 |
| mean anomaly at epoch: | 292.9018° |
| orbit number at epoch: | 52868 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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