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 38738U 12042A 12333.60875234 +.00013656 +00000-0 +23040-3 0 9998
2 38738 051.6499 024.7441 0015766 340.1845 155.9317 15.51837211018449
| Epoch (UTC): | 28 November 2012 14:36:36 |
| Eccentricity: | 0.0015766 |
| inclination: | 51.6499° |
| perigee height: | 400 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 24.7441° |
| argument of perigee: | 340.1845° |
| revolutions per day: | 15.51837211 |
| mean anomaly at epoch: | 155.9317° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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