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 28521U 05002A 19082.78319682 .00000038 00000-0 18762-4 0 9998
2 28521 82.9470 241.5264 0039333 303.7471 55.9949 13.87608630717671
| Epoch (UTC): | 23 March 2019 18:47:48 |
| Eccentricity: | 0.0039333 |
| inclination: | 82.9470° |
| perigee height: | 908 km |
| apogee height: | 966 km |
| right ascension of ascending node: | 241.5264° |
| argument of perigee: | 303.7471° |
| revolutions per day: | 13.87608630 |
| mean anomaly at epoch: | 55.9949° |
| orbit number at epoch: | 71767 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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