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 64183U 26145.27802575 +.00000000 +00000-0 +57427-3 0 00007
2 64183 53.1578 95.2093 0001241 92.9341 267.1803 15.31723374 00
| Epoch (UTC): | 25 May 2026 06:40:21 |
| Eccentricity: | 0.0001241 |
| inclination: | 53.1578° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 95.2093° |
| argument of perigee: | 92.9341° |
| revolutions per day: | 15.31723374 |
| mean anomaly at epoch: | 267.1803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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