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 25064U 97074B 13143.80041841 .00010087 00000-0 26934-3 0 9018
2 25064 034.9698 270.4428 0005383 019.3814 101.7040 15.37287800861021
| Epoch (UTC): | 23 May 2013 19:12:36 |
| Eccentricity: | 0.0005383 |
| inclination: | 34.9698° |
| perigee height: | 450 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 270.4428° |
| argument of perigee: | 19.3814° |
| revolutions per day: | 15.37287800 |
| mean anomaly at epoch: | 101.7040° |
| orbit number at epoch: | 86102 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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