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 12904U 81103B 13142.46643060 .00001431 00000-0 10963-3 0 2353
2 12904 081.1777 169.0183 0029556 264.6969 095.0878 15.00941394269411
| Epoch (UTC): | 22 May 2013 11:11:39 |
| Eccentricity: | 0.0029556 |
| inclination: | 81.1777° |
| perigee height: | 543 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 169.0183° |
| argument of perigee: | 264.6969° |
| revolutions per day: | 15.00941394 |
| mean anomaly at epoch: | 95.0878° |
| orbit number at epoch: | 26941 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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