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 56209U 26145.53126000 +.00000000 +00000-0 +19479-3 0 00003
2 56209 97.3024 53.6215 0009823 111.2145 249.0156 15.49331587 01
| Epoch (UTC): | 25 May 2026 12:45:00 |
| Eccentricity: | 0.0009823 |
| inclination: | 97.3024° |
| perigee height: | 412 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 53.6215° |
| argument of perigee: | 111.2145° |
| revolutions per day: | 15.49331587 |
| mean anomaly at epoch: | 249.0156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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