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 23340.15602590 .00001771 00000-0 31009-3 0 9991
2 27939 98.2649 128.7388 0011498 317.4715 129.3635 14.69061452 79786
| Epoch (UTC): | 06 December 2023 03:44:40 |
| Eccentricity: | 0.0011498 |
| inclination: | 98.2649° |
| perigee height: | 656 km |
| apogee height: | 672 km |
| right ascension of ascending node: | 128.7388° |
| argument of perigee: | 317.4715° |
| revolutions per day: | 14.69061452 |
| mean anomaly at epoch: | 129.3635° |
| orbit number at epoch: | 7978 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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