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 26874U 01032B 13140.18526462 .00008928 00000-0 19047-3 0 3812
2 26874 082.4783 032.1447 0019815 047.7003 312.5920 15.44490058660517
| Epoch (UTC): | 20 May 2013 04:26:46 |
| Eccentricity: | 0.0019815 |
| inclination: | 82.4783° |
| perigee height: | 419 km |
| apogee height: | 446 km |
| right ascension of ascending node: | 32.1447° |
| argument of perigee: | 47.7003° |
| revolutions per day: | 15.44490058 |
| mean anomaly at epoch: | 312.5920° |
| orbit number at epoch: | 66051 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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