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 23468U 95003B 13142.50291015 .00004748 00000-0 11699-2 0 761
2 23468 026.7520 292.6662 6222897 356.5377 017.8784 03.70543595224624
| Epoch (UTC): | 22 May 2013 12:04:11 |
| Eccentricity: | 0.6222897 |
| inclination: | 26.7520° |
| perigee height: | 285 km |
| apogee height: | 22239 km |
| right ascension of ascending node: | 292.6662° |
| argument of perigee: | 356.5377° |
| revolutions per day: | 3.70543595 |
| mean anomaly at epoch: | 17.8784° |
| orbit number at epoch: | 22462 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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