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 23337.85241270 .00004881 00000-0 60801-3 0 9992
2 39440 97.7927 281.3881 0072344 193.5803 166.3465 14.81065885540458
| Epoch (UTC): | 03 December 2023 20:27:28 |
| Eccentricity: | 0.0072344 |
| inclination: | 97.7927° |
| perigee height: | 575 km |
| apogee height: | 676 km |
| right ascension of ascending node: | 281.3881° |
| argument of perigee: | 193.5803° |
| revolutions per day: | 14.81065885 |
| mean anomaly at epoch: | 166.3465° |
| orbit number at epoch: | 54045 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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