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 data is extracted from the following two-line orbital elements,
1 39092U 13009G 15060.54649223 .00000241 00000-0 10067-3 0 9997
2 39092 098.6096 259.3154 0008334 265.7780 094.2453 14.34708843105213
| Epoch (UTC): | 01 March 2015 13:06:56 |
| Eccentricity: | 0.0008334 |
| inclination: | 98.6096° |
| perigee height: | 770 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 259.3154° |
| argument of perigee: | 265.7780° |
| revolutions per day: | 14.34708843 |
| mean anomaly at epoch: | 94.2453° |
| orbit number at epoch: | 10521 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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