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 25578U 98074B 13144.53331017 .00000144 00000-0 44400-4 0 4137
2 25578 086.3971 156.2010 0002602 105.5729 040.8199 14.34213654764604
| Epoch (UTC): | 24 May 2013 12:47:57 |
| Eccentricity: | 0.0002602 |
| inclination: | 86.3971° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 156.2010° |
| argument of perigee: | 105.5729° |
| revolutions per day: | 14.34213654 |
| mean anomaly at epoch: | 40.8199° |
| orbit number at epoch: | 76460 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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