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 56554U 26145.48010084 +.00000000 +00000-0 +28282-4 0 00007
2 56554 43.0036 150.1291 0001791 269.6935 90.3712 15.27578922 00
| Epoch (UTC): | 25 May 2026 11:31:20 |
| Eccentricity: | 0.0001791 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 150.1291° |
| argument of perigee: | 269.6935° |
| revolutions per day: | 15.27578922 |
| mean anomaly at epoch: | 90.3712° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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