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 25274U 98019C 13143.23986005 .00000324 00000-0 10855-3 0 1108
2 25274 086.3989 188.5034 0002381 110.9787 249.1664 14.34223055793089
| Epoch (UTC): | 23 May 2013 05:45:23 |
| Eccentricity: | 0.0002381 |
| inclination: | 86.3989° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 188.5034° |
| argument of perigee: | 110.9787° |
| revolutions per day: | 14.34223055 |
| mean anomaly at epoch: | 249.1664° |
| orbit number at epoch: | 79308 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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