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 26145.93820036 +.00000000 +00000-0 +94859-4 0 00009
2 20547 94.0864 130.9239 0053793 217.0648 142.6888 15.43869075 08
| Epoch (UTC): | 25 May 2026 22:31:00 |
| Eccentricity: | 0.0053793 |
| inclination: | 94.0864° |
| perigee height: | 398 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 130.9239° |
| argument of perigee: | 217.0648° |
| revolutions per day: | 15.43869075 |
| mean anomaly at epoch: | 142.6888° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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