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 32785U 08021C 21016.82844411 .00000235 00000-0 30863-4 0 9992
2 32785 97.5947 1.7202 0013858 140.6683 219.5543 14.88612193689615
| Epoch (UTC): | 16 January 2021 19:52:57 |
| Eccentricity: | 0.0013858 |
| inclination: | 97.5947° |
| perigee height: | 592 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 1.7202° |
| argument of perigee: | 140.6683° |
| revolutions per day: | 14.88612193 |
| mean anomaly at epoch: | 219.5543° |
| orbit number at epoch: | 68961 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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