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 34602U 09013A 13314.96046236 .14220718 20669-5 50412-4 0 9995
2 34602 096.5717 344.5256 0009826 296.2811 064.0942 16.58673376272979
Epoch (UTC): | 10 November 2013 23:03:03 |
Eccentricity: | 0.0009826 |
inclination: | 96.5717° |
perigee height: | 110 km |
apogee height: | 123 km |
right ascension of ascending node: | 344.5256° |
argument of perigee: | 296.2811° |
revolutions per day: | 16.58673376 |
mean anomaly at epoch: | 64.0942° |
orbit number at epoch: | 27297 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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