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 37874U 11066A 16037.88394846 +.05602070 +24770-5 +25199-3 0 9994
2 37874 097.2929 156.3903 0010482 290.5862 070.4403 16.42369431239565
| Epoch (UTC): | 06 February 2016 21:12:53 |
| Eccentricity: | 0.0010482 |
| inclination: | 97.2929° |
| perigee height: | 152 km |
| apogee height: | 166 km |
| right ascension of ascending node: | 156.3903° |
| argument of perigee: | 290.5862° |
| revolutions per day: | 16.42369431 |
| mean anomaly at epoch: | 70.4403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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