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 30587U 07005B 13198.07262483 0.00048000 00000-0 54274-3 0 09
2 30587 97.4155 343.2231 0003000 71.2924 288.7075 15.62435735 00
| Epoch (UTC): | 17 July 2013 01:44:34 |
| Eccentricity: | 0.0003000 |
| inclination: | 97.4155° |
| perigee height: | 378 km |
| apogee height: | 382 km |
| right ascension of ascending node: | 343.2231° |
| argument of perigee: | 71.2924° |
| revolutions per day: | 15.62435735 |
| mean anomaly at epoch: | 288.7075° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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