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 25342U 98032A 13170.44426155 .00000226 00000-0 73539-4 0 3626
2 25342 086.3992 113.9362 0002514 101.6279 037.1280 14.34219764790017
| Epoch (UTC): | 19 June 2013 10:39:44 |
| Eccentricity: | 0.0002514 |
| inclination: | 86.3992° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 113.9362° |
| argument of perigee: | 101.6279° |
| revolutions per day: | 14.34219764 |
| mean anomaly at epoch: | 37.1280° |
| orbit number at epoch: | 79001 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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