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 38081U 12006E 15009.86954674 .36181825 49011-5 43735-3 0 9992
2 38081 069.4150 141.5751 0006093 101.2598 259.4750 16.49686879155248
| Epoch (UTC): | 09 January 2015 20:52:08 |
| Eccentricity: | 0.0006093 |
| inclination: | 69.4150° |
| perigee height: | 136 km |
| apogee height: | 144 km |
| right ascension of ascending node: | 141.5751° |
| argument of perigee: | 101.2598° |
| revolutions per day: | 16.49686879 |
| mean anomaly at epoch: | 259.4750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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