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 38975U 12060A 13111.57604513 -.00391701 00000-0 -44465-2 0 9997
2 38975 051.6532 028.8472 0041788 317.8087 042.1803 15.61650999 26769
| Epoch (UTC): | 21 April 2013 13:49:30 |
| Eccentricity: | 0.0041788 |
| inclination: | 51.6532° |
| perigee height: | 354 km |
| apogee height: | 411 km |
| right ascension of ascending node: | 28.8472° |
| argument of perigee: | 317.8087° |
| revolutions per day: | 15.61650999 |
| mean anomaly at epoch: | 42.1803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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