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 37375U 11010A 12151.09943120 0.00000000 00000-0 00000-0 0 09
2 37375 41.8922 42.5837 0008151 3.7995 356.1998 15.96578464 06
| Epoch (UTC): | 30 May 2012 02:23:10 |
| Eccentricity: | 0.0008151 |
| inclination: | 41.8922° |
| perigee height: | 278 km |
| apogee height: | 289 km |
| right ascension of ascending node: | 42.5837° |
| argument of perigee: | 3.7995° |
| revolutions per day: | 15.96578464 |
| mean anomaly at epoch: | 356.1998° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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