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 26473U 00047A 14056.12432529 0.00000300 00000-0 55593-4 0 04
2 26473 68.0114 73.0137 0005000 177.1720 182.8280 14.65191444 03
Epoch (UTC): | 25 February 2014 02:59:01 |
Eccentricity: | 0.0005000 |
inclination: | 68.0114° |
perigee height: | 673 km |
apogee height: | 680 km |
right ascension of ascending node: | 73.0137° |
argument of perigee: | 177.1720° |
revolutions per day: | 14.65191444 |
mean anomaly at epoch: | 182.8280° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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