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 18170.82275304 -.00000242 +00000-0 +00000-0 0 9999
2 26609 006.0612 147.0501 7959964 261.9656 011.6516 01.25588589080843
| Epoch (UTC): | 19 June 2018 19:44:45 |
| Eccentricity: | 0.7959964 |
| inclination: | 6.0612° |
| perigee height: | 1025 km |
| apogee height: | 58795 km |
| right ascension of ascending node: | 147.0501° |
| argument of perigee: | 261.9656° |
| revolutions per day: | 1.25588589 |
| mean anomaly at epoch: | 11.6516° |
| orbit number at epoch: | 8084 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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