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 38085U 12006J 15047.13271005 .15174231 50628-5 38163-3 0 9993
2 38085 069.4022 049.8202 0017770 344.8867 016.3100 16.44194733160691
| Epoch (UTC): | 16 February 2015 03:11:06 |
| Eccentricity: | 0.0017770 |
| inclination: | 69.4022° |
| perigee height: | 143 km |
| apogee height: | 166 km |
| right ascension of ascending node: | 49.8202° |
| argument of perigee: | 344.8867° |
| revolutions per day: | 16.44194733 |
| mean anomaly at epoch: | 16.3100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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