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 32958U 08026A 17170.68112436 +.00000007 +00000-0 +22788-4 0 9998
2 32958 098.4089 199.2336 0008550 278.2925 081.7214 14.19664016469687
| Epoch (UTC): | 19 June 2017 16:20:49 |
| Eccentricity: | 0.0008550 |
| inclination: | 98.4089° |
| perigee height: | 820 km |
| apogee height: | 832 km |
| right ascension of ascending node: | 199.2336° |
| argument of perigee: | 278.2925° |
| revolutions per day: | 14.19664016 |
| mean anomaly at epoch: | 81.7214° |
| orbit number at epoch: | 46968 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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