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 19650U 88102B 13168.54150112 .00000089 00000-0 69859-4 0 302
2 19650 070.9979 206.1077 0016167 249.1583 215.9813 14.15613820269276
| Epoch (UTC): | 17 June 2013 12:59:45 |
| Eccentricity: | 0.0016167 |
| inclination: | 70.9979° |
| perigee height: | 828 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 206.1077° |
| argument of perigee: | 249.1583° |
| revolutions per day: | 14.15613820 |
| mean anomaly at epoch: | 215.9813° |
| orbit number at epoch: | 26927 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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