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 13142.15116530 .00000433 00000-0 10614-3 0 1577
2 25682 098.1932 211.9690 0001144 115.3214 244.8115 14.57119414750040
| Epoch (UTC): | 22 May 2013 03:37:40 |
| Eccentricity: | 0.0001144 |
| inclination: | 98.1932° |
| perigee height: | 701 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 211.9690° |
| argument of perigee: | 115.3214° |
| revolutions per day: | 14.57119414 |
| mean anomaly at epoch: | 244.8115° |
| orbit number at epoch: | 75004 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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