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 00047U 60007C 18171.46235240 -.00000038 00000-0 16486-4 0 9999
2 00047 66.6665 301.3880 0221001 116.7600 245.6303 14.41987593 30162
| Epoch (UTC): | 20 June 2018 11:05:47 |
| Eccentricity: | 0.0221001 |
| inclination: | 66.6665° |
| perigee height: | 594 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 301.3880° |
| argument of perigee: | 116.7600° |
| revolutions per day: | 14.41987593 |
| mean anomaly at epoch: | 245.6303° |
| orbit number at epoch: | 3016 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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