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 61926U 26144.90346294 +.00000000 +00000-0 +83031-3 0 00009
2 61926 43.0006 210.8444 0001800 274.7748 85.2898 15.27615822 09
| Epoch (UTC): | 24 May 2026 21:40:59 |
| Eccentricity: | 0.0001800 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 210.8444° |
| argument of perigee: | 274.7748° |
| revolutions per day: | 15.27615822 |
| mean anomaly at epoch: | 85.2898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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