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 56911U 26145.27852279 +.00000000 +00000-0 +17199-4 0 00006
2 56911 43.0018 357.9585 0001130 246.1634 113.9099 15.27577722 00
| Epoch (UTC): | 25 May 2026 06:41:04 |
| Eccentricity: | 0.0001130 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 357.9585° |
| argument of perigee: | 246.1634° |
| revolutions per day: | 15.27577722 |
| mean anomaly at epoch: | 113.9099° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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