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 59042U 26145.51241285 +.00000000 +00000-0 +33257-3 0 00002
2 59042 43.0040 309.1732 0002421 338.4669 21.6081 15.27627030 07
| Epoch (UTC): | 25 May 2026 12:17:52 |
| Eccentricity: | 0.0002421 |
| inclination: | 43.0040° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 309.1732° |
| argument of perigee: | 338.4669° |
| revolutions per day: | 15.27627030 |
| mean anomaly at epoch: | 21.6081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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