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 40661U 15025L 15164.02321742 0.06860311 00000-0 77534-1 0 03
2 40661 54.9961 238.2507 0124429 247.3969 111.3864 15.52760368 09
| Epoch (UTC): | 13 June 2015 00:33:25 |
| Eccentricity: | 0.0124429 |
| inclination: | 54.9961° |
| perigee height: | 324 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 238.2507° |
| argument of perigee: | 247.3969° |
| revolutions per day: | 15.52760368 |
| mean anomaly at epoch: | 111.3864° |
| 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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