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 25994U 99068A 14114.81427755 .00000764 00000-0 17957-3 0 1745
2 25994 098.2137 190.2794 0001553 108.7970 251.3353 14.57139861763293
| Epoch (UTC): | 24 April 2014 19:32:33 |
| Eccentricity: | 0.0001553 |
| inclination: | 98.2137° |
| perigee height: | 701 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 190.2794° |
| argument of perigee: | 108.7970° |
| revolutions per day: | 14.57139861 |
| mean anomaly at epoch: | 251.3353° |
| orbit number at epoch: | 76329 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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