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 56022U 26145.21627352 +.00000000 +00000-0 +12735-4 0 00006
2 56022 43.0032 332.6701 0001288 269.4855 90.5850 15.27576649 08
| Epoch (UTC): | 25 May 2026 05:11:26 |
| Eccentricity: | 0.0001288 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 332.6701° |
| argument of perigee: | 269.4855° |
| revolutions per day: | 15.27576649 |
| mean anomaly at epoch: | 90.5850° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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