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 20547U 26140.42862454 +.00000000 +00000-0 +71893-4 0 00001
2 20547 94.0871 127.8226 0053149 239.0678 120.5348 15.43825253 05
| Epoch (UTC): | 20 May 2026 10:17:13 |
| Eccentricity: | 0.0053149 |
| inclination: | 94.0871° |
| perigee height: | 399 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 127.8226° |
| argument of perigee: | 239.0678° |
| revolutions per day: | 15.43825253 |
| mean anomaly at epoch: | 120.5348° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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