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 13168.46533068 .00000316 00000-0 22791-4 0 2542
2 12904 081.1790 139.5291 0031091 178.2585 181.8750 15.01005265273315
| Epoch (UTC): | 17 June 2013 11:10:04 |
| Eccentricity: | 0.0031091 |
| inclination: | 81.1790° |
| perigee height: | 542 km |
| apogee height: | 585 km |
| right ascension of ascending node: | 139.5291° |
| argument of perigee: | 178.2585° |
| revolutions per day: | 15.01005265 |
| mean anomaly at epoch: | 181.8750° |
| orbit number at epoch: | 27331 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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