Genesis I - Orbit

View from above orbital plane
View from above orbital plane
View from above satellite
View from above satellite

Ground track
Ground track

The orbit data is extracted from the following two-line orbital elements,

1 29252U 06029A   13140.37561336  .00003391  00000-0  23246-3 0  8995
2 29252 064.5105 080.8411 0012670 203.9173 302.0836 15.07742185376565
Epoch (UTC): 20 May 2013 09:00:52
Eccentricity: 0.0012670
inclination: 64.5105°
perigee height: 534 km
apogee height: 552 km
right ascension of ascending node: 80.8411°
argument of perigee: 203.9173°
revolutions per day: 15.07742185
mean anomaly at epoch: 302.0836°
orbit number at epoch: 37656

The dashed part of the orbit path shows where the satellite is in the earth's shadow,  

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