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 56291U 26145.34080501 +.00000000 +00000-0 -43483-4 0 00002
2 56291 43.0017 135.9574 0000507 276.6001 83.4793 15.27595567 04
| Epoch (UTC): | 25 May 2026 08:10:45 |
| Eccentricity: | 0.0000507 |
| inclination: | 43.0017° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 135.9574° |
| argument of perigee: | 276.6001° |
| revolutions per day: | 15.27595567 |
| mean anomaly at epoch: | 83.4793° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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