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 20547U 90028B 17173.58281038 +.00000234 +00000-0 +97288-5 0 9999
2 20547 094.1034 131.9849 0082272 239.5304 119.7797 15.23886045500001
| Epoch (UTC): | 22 June 2017 13:59:14 |
| Eccentricity: | 0.0082272 |
| inclination: | 94.1034° |
| perigee height: | 437 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 131.9849° |
| argument of perigee: | 239.5304° |
| revolutions per day: | 15.23886045 |
| mean anomaly at epoch: | 119.7797° |
| orbit number at epoch: | 50000 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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