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 19082.10130016 -.00000082 00000-0 00000+0 0 9994
2 26609 8.0105 85.4552 7974423 9.7954 359.3019 1.25587512 84433
| Epoch (UTC): | 23 March 2019 02:25:52 |
| Eccentricity: | 0.7974423 |
| inclination: | 8.0105° |
| perigee height: | 972 km |
| apogee height: | 58848 km |
| right ascension of ascending node: | 85.4552° |
| argument of perigee: | 9.7954° |
| revolutions per day: | 1.25587512 |
| mean anomaly at epoch: | 359.3019° |
| orbit number at epoch: | 8443 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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