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 15392U 84115B 17174.77143848 +.00000124 +00000-0 -21642-4 0 9998
2 15392 021.4904 281.0500 1034617 078.6987 292.7720 12.45548213467040
| Epoch (UTC): | 23 June 2017 18:30:52 |
| Eccentricity: | 0.1034617 |
| inclination: | 21.4904° |
| perigee height: | 670 km |
| apogee height: | 2296 km |
| right ascension of ascending node: | 281.0500° |
| argument of perigee: | 78.6987° |
| revolutions per day: | 12.45548213 |
| mean anomaly at epoch: | 292.7720° |
| orbit number at epoch: | 46704 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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