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 26609U 00072B 18344.38787669 -.00000283 00000-0 00000+0 0 9999
2 26609 6.9595 104.6843 7987074 333.3735 1.8626 1.25587822 83143
| Epoch (UTC): | 10 December 2018 09:18:32 |
| Eccentricity: | 0.7987074 |
| inclination: | 6.9595° |
| perigee height: | 926 km |
| apogee height: | 58894 km |
| right ascension of ascending node: | 104.6843° |
| argument of perigee: | 333.3735° |
| revolutions per day: | 1.25587822 |
| mean anomaly at epoch: | 1.8626° |
| orbit number at epoch: | 8314 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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