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 25682U 99020A 13140.70911112 .00000463 00000-0 11284-3 0 1538
2 25682 098.1933 210.5498 0001159 119.0473 241.0837 14.57118090749830
| Epoch (UTC): | 20 May 2013 17:01:07 |
| Eccentricity: | 0.0001159 |
| inclination: | 98.1933° |
| perigee height: | 701 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 210.5498° |
| argument of perigee: | 119.0473° |
| revolutions per day: | 14.57118090 |
| mean anomaly at epoch: | 241.0837° |
| orbit number at epoch: | 74983 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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