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 39266U 26142.93810094 +.00000000 +00000-0 +80889-4 0 00005
2 39266 80.9009 14.9997 0019790 258.9644 100.9431 16.54176160 02
| Epoch (UTC): | 22 May 2026 22:30:51 |
| Eccentricity: | 0.0019790 |
| inclination: | 80.9009° |
| perigee height: | 115 km |
| apogee height: | 141 km |
| right ascension of ascending node: | 14.9997° |
| argument of perigee: | 258.9644° |
| revolutions per day: | 16.54176160 |
| mean anomaly at epoch: | 100.9431° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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