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 25290U 98021F 13139.47820078 .00000188 00000-0 60079-4 0 681
2 25290 086.3958 126.6112 0002270 104.7962 255.3486 14.34218695791506
| Epoch (UTC): | 19 May 2013 11:28:36 |
| Eccentricity: | 0.0002270 |
| inclination: | 86.3958° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 126.6112° |
| argument of perigee: | 104.7962° |
| revolutions per day: | 14.34218695 |
| mean anomaly at epoch: | 255.3486° |
| orbit number at epoch: | 79150 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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