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 40897U 98067GX 16087.17198643 .14496049 12607-4 75186-3 0 9996
2 40897 51.6079 83.5146 0009266 349.7464 11.2974 16.42052915 30018
| Epoch (UTC): | 27 March 2016 04:07:39 |
| Eccentricity: | 0.0009266 |
| inclination: | 51.6079° |
| perigee height: | 154 km |
| apogee height: | 166 km |
| right ascension of ascending node: | 83.5146° |
| argument of perigee: | 349.7464° |
| revolutions per day: | 16.42052915 |
| mean anomaly at epoch: | 11.2974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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