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 26635U 00080A 19030.42692377 0.00000000 00000-0 00000-0 0 06
2 26635 8.5911 33.0327 0007880 204.6175 155.3561 1.00270000 00
| Epoch (UTC): | 30 January 2019 10:14:46 |
| Eccentricity: | 0.0007880 |
| inclination: | 8.5911° |
| perigee height: | 35753 km |
| apogee height: | 35820 km |
| right ascension of ascending node: | 33.0327° |
| argument of perigee: | 204.6175° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 155.3561° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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