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 59789U 26145.42026623 +.00000000 +00000-0 +21168-4 0 00006
2 59789 43.0026 135.2856 0000918 283.6480 76.4269 15.27575191 01
| Epoch (UTC): | 25 May 2026 10:05:11 |
| Eccentricity: | 0.0000918 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 135.2856° |
| argument of perigee: | 283.6480° |
| revolutions per day: | 15.27575191 |
| mean anomaly at epoch: | 76.4269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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