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 27939U 03042A 23333.47142984 .00002699 00000-0 46825-3 0 9996
2 27939 98.2644 121.9782 0011826 339.6341 56.3297 14.69030166 78803
| Epoch (UTC): | 29 November 2023 11:18:51 |
| Eccentricity: | 0.0011826 |
| inclination: | 98.2644° |
| perigee height: | 656 km |
| apogee height: | 672 km |
| right ascension of ascending node: | 121.9782° |
| argument of perigee: | 339.6341° |
| revolutions per day: | 14.69030166 |
| mean anomaly at epoch: | 56.3297° |
| orbit number at epoch: | 7880 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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