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 13141.25846515 .00000498 00000-0 12047-3 0 1551
2 25682 098.1932 211.0905 0001160 117.3366 242.7946 14.57118761749915
| Epoch (UTC): | 21 May 2013 06:12:11 |
| Eccentricity: | 0.0001160 |
| inclination: | 98.1932° |
| perigee height: | 701 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 211.0905° |
| argument of perigee: | 117.3366° |
| revolutions per day: | 14.57118761 |
| mean anomaly at epoch: | 242.7946° |
| orbit number at epoch: | 74991 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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