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 23332.85281479 .00005746 00000-0 71587-3 0 9996
2 39440 97.7923 276.5278 0072023 210.0805 149.6263 14.81004507538519
| Epoch (UTC): | 28 November 2023 20:28:03 |
| Eccentricity: | 0.0072023 |
| inclination: | 97.7923° |
| perigee height: | 576 km |
| apogee height: | 676 km |
| right ascension of ascending node: | 276.5278° |
| argument of perigee: | 210.0805° |
| revolutions per day: | 14.81004507 |
| mean anomaly at epoch: | 149.6263° |
| orbit number at epoch: | 53851 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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