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 26621U 00075C 19340.87742808 +.00000634 +00000-0 +59859-3 0 9992
2 26621 095.3940 323.0820 0711045 273.0990 078.9067 13.04168256906058
| Epoch (UTC): | 06 December 2019 21:03:29 |
| Eccentricity: | 0.0711045 |
| inclination: | 95.3940° |
| perigee height: | 704 km |
| apogee height: | 1788 km |
| right ascension of ascending node: | 323.0820° |
| argument of perigee: | 273.0990° |
| revolutions per day: | 13.04168256 |
| mean anomaly at epoch: | 78.9067° |
| orbit number at epoch: | 90605 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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