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 39168U 26140.44004692 +.00000000 +00000-0 +00000-0 0 00002
2 39168 0.0185 287.3810 0000293 24.2400 32.3821 1.00273178 06
| Epoch (UTC): | 20 May 2026 10:33:40 |
| Eccentricity: | 0.0000293 |
| inclination: | 0.0185° |
| perigee height: | 35785 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 287.3810° |
| argument of perigee: | 24.2400° |
| revolutions per day: | 1.00273178 |
| mean anomaly at epoch: | 32.3821° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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