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 14203.97001004 .00000215 00000-0 91847-4 0 4285
2 39092 098.6200 038.3757 0009064 196.4824 163.6066 14.34580168 73453
| Epoch (UTC): | 22 July 2014 23:16:48 |
| Eccentricity: | 0.0009064 |
| inclination: | 98.6200° |
| perigee height: | 770 km |
| apogee height: | 783 km |
| right ascension of ascending node: | 38.3757° |
| argument of perigee: | 196.4824° |
| revolutions per day: | 14.34580168 |
| mean anomaly at epoch: | 163.6066° |
| orbit number at epoch: | 7345 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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