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 is defined by the following mean orbital elements,
1 38073U 12004A 12119.55885225 .00321465 00000-0 35762-2 0 9998
2 38073 051.6442 010.6074 0048899 338.9495 021.1673 15.59843058 14612
| Epoch (UTC): | 28 April 2012 13:24:44 |
| Eccentricity: | 0.0048899 |
| inclination: | 51.6442° |
| perigee height: | 355 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 10.6074° |
| argument of perigee: | 338.9495° |
| revolutions per day: | 15.59843058 |
| mean anomaly at epoch: | 21.1673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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