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 is defined by the following mean orbital elements,
1 27392U 02012B 17357.93734954 .20424135 -59216-6 17216-3 0 9996
2 27392 88.9684 292.6153 0002005 198.7136 161.7226 16.52514316887583
| Epoch (UTC): | 23 December 2017 22:29:47 |
| Eccentricity: | 0.0002005 |
| inclination: | 88.9684° |
| perigee height: | 131 km |
| apogee height: | 134 km |
| right ascension of ascending node: | 292.6153° |
| argument of perigee: | 198.7136° |
| revolutions per day: | 16.52514316 |
| mean anomaly at epoch: | 161.7226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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