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 38083U 12006G 14301.11956501 .22610689 46455-5 46708-3 0 9999
2 38083 069.4009 319.6607 0016614 123.6531 236.4095 16.45428332144559
| Epoch (UTC): | 28 October 2014 02:52:10 |
| Eccentricity: | 0.0016614 |
| inclination: | 69.4009° |
| perigee height: | 140 km |
| apogee height: | 162 km |
| right ascension of ascending node: | 319.6607° |
| argument of perigee: | 123.6531° |
| revolutions per day: | 16.45428332 |
| mean anomaly at epoch: | 236.4095° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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