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 64578U 26145.59892656 +.00000000 +00000-0 +34597-3 0 00002
2 64578 97.7872 262.0052 0001768 51.9291 308.2092 15.00860658 01
| Epoch (UTC): | 25 May 2026 14:22:27 |
| Eccentricity: | 0.0001768 |
| inclination: | 97.7872° |
| perigee height: | 563 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 262.0052° |
| argument of perigee: | 51.9291° |
| revolutions per day: | 15.00860658 |
| mean anomaly at epoch: | 308.2092° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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