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 24251.84860594 .00017726 00000-0 20109-2 0 9991
2 39440 97.8163 193.8063 0068285 5.8154 354.3838 14.84689140581797
| Epoch (UTC): | 07 September 2024 20:21:59 |
| Eccentricity: | 0.0068285 |
| inclination: | 97.8163° |
| perigee height: | 567 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 193.8063° |
| argument of perigee: | 5.8154° |
| revolutions per day: | 14.84689140 |
| mean anomaly at epoch: | 354.3838° |
| orbit number at epoch: | 58179 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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