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 16262U 85108A 13143.10044457 .00002296 00000-0 16758-3 0 1706
2 16262 082.4953 261.5380 0012574 000.0216 000.1008 15.03185369495001
| Epoch (UTC): | 23 May 2013 02:24:38 |
| Eccentricity: | 0.0012574 |
| inclination: | 82.4953° |
| perigee height: | 548 km |
| apogee height: | 566 km |
| right ascension of ascending node: | 261.5380° |
| argument of perigee: | 0.0216° |
| revolutions per day: | 15.03185369 |
| mean anomaly at epoch: | 0.1008° |
| orbit number at epoch: | 49500 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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