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 55456U 26145.32710480 +.00000000 +00000-0 +32900-4 0 00009
2 55456 43.0011 255.8403 0001301 275.7930 84.2773 15.27578740 08
| Epoch (UTC): | 25 May 2026 07:51:01 |
| Eccentricity: | 0.0001301 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 255.8403° |
| argument of perigee: | 275.7930° |
| revolutions per day: | 15.27578740 |
| mean anomaly at epoch: | 84.2773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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