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 37802U 11046B 11253.59467199 +.00002457 -77678-5 +00000-0 0 9993
2 37802 028.5000 009.1212 0000200 263.4759 096.5843 16.41337653000015
| Epoch (UTC): | 10 September 2011 14:16:19 |
| Eccentricity: | 0.0000200 |
| inclination: | 28.5000° |
| perigee height: | 162 km |
| apogee height: | 162 km |
| right ascension of ascending node: | 9.1212° |
| argument of perigee: | 263.4759° |
| revolutions per day: | 16.41337653 |
| mean anomaly at epoch: | 96.5843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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