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 39388U 13064J 15080.71275061 .12341207 73157-5 15275-2 0 9998
2 39388 040.5115 217.0045 0004625 328.4988 031.6239 16.35091082 75042
| Epoch (UTC): | 21 March 2015 17:06:21 |
| Eccentricity: | 0.0004625 |
| inclination: | 40.5115° |
| perigee height: | 176 km |
| apogee height: | 182 km |
| right ascension of ascending node: | 217.0045° |
| argument of perigee: | 328.4988° |
| revolutions per day: | 16.35091082 |
| mean anomaly at epoch: | 31.6239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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