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 27844U 03031E 19082.90567808 +.00000027 +00000-0 +31938-4 0 9992
2 27844 098.6869 092.4064 0008676 283.8705 076.1507 14.22166063815919
| Epoch (UTC): | 23 March 2019 21:44:10 |
| Eccentricity: | 0.0008676 |
| inclination: | 98.6869° |
| perigee height: | 812 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 92.4064° |
| argument of perigee: | 283.8705° |
| revolutions per day: | 14.22166063 |
| mean anomaly at epoch: | 76.1507° |
| orbit number at epoch: | 81591 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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