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 38084U 12006H 15027.67615865 .06348435 00000-0 93957-3 0 9990
2 38084 069.3936 096.9914 0019855 020.5600 339.7407 16.33497838157862
| Epoch (UTC): | 27 January 2015 16:13:40 |
| Eccentricity: | 0.0019855 |
| inclination: | 69.3936° |
| perigee height: | 170 km |
| apogee height: | 196 km |
| right ascension of ascending node: | 96.9914° |
| argument of perigee: | 20.5600° |
| revolutions per day: | 16.33497838 |
| mean anomaly at epoch: | 339.7407° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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