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 is defined by the following mean orbital elements,
1 13526U 74089EM 19230.04374589 -.00000029 00000-0 34319-4 0 9996
2 13526 101.1740 317.5017 0475814 76.1490 289.2004 11.89642017 52497
| Epoch (UTC): | 18 August 2019 01:02:59 |
| Eccentricity: | 0.0475814 |
| inclination: | 101.1740° |
| perigee height: | 1342 km |
| apogee height: | 2113 km |
| right ascension of ascending node: | 317.5017° |
| argument of perigee: | 76.1490° |
| revolutions per day: | 11.89642017 |
| mean anomaly at epoch: | 289.2004° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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