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 data is extracted from the following two-line orbital elements,
1 39170U 13025A 13149.11632458 .00010281 00000-0 18396-3 0 37
2 39170 051.6489 202.9048 0009929 010.2269 092.6265 15.50570246 37
| Epoch (UTC): | 29 May 2013 02:47:30 |
| Eccentricity: | 0.0009929 |
| inclination: | 51.6489° |
| perigee height: | 408 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 202.9048° |
| argument of perigee: | 10.2269° |
| revolutions per day: | 15.50570246 |
| mean anomaly at epoch: | 92.6265° |
| orbit number at epoch: | 3 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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