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 23339.54142686 .00003752 00000-0 46883-3 0 9991
2 39440 97.7928 283.0304 0072514 188.0523 171.9532 14.81077836539505
| Epoch (UTC): | 05 December 2023 12:59:39 |
| Eccentricity: | 0.0072514 |
| inclination: | 97.7928° |
| perigee height: | 575 km |
| apogee height: | 677 km |
| right ascension of ascending node: | 283.0304° |
| argument of perigee: | 188.0523° |
| revolutions per day: | 14.81077836 |
| mean anomaly at epoch: | 171.9532° |
| orbit number at epoch: | 53950 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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