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 57056U 26144.97991573 +.00000000 +00000-0 +64623-4 0 00008
2 57056 43.0056 39.5036 0001329 249.2012 110.8697 15.27572105 01
| Epoch (UTC): | 24 May 2026 23:31:04 |
| Eccentricity: | 0.0001329 |
| inclination: | 43.0056° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 39.5036° |
| argument of perigee: | 249.2012° |
| revolutions per day: | 15.27572105 |
| mean anomaly at epoch: | 110.8697° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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