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 42806U 26145.23939323 +.00000000 +00000-0 -32725-5 0 00000
2 42806 86.4483 331.6864 0002105 82.4380 277.7060 14.43280340 07
| Epoch (UTC): | 25 May 2026 05:44:43 |
| Eccentricity: | 0.0002105 |
| inclination: | 86.4483° |
| perigee height: | 746 km |
| apogee height: | 749 km |
| right ascension of ascending node: | 331.6864° |
| argument of perigee: | 82.4380° |
| revolutions per day: | 14.43280340 |
| mean anomaly at epoch: | 277.7060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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