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 59743U 26145.27444639 +.00000000 +00000-0 +22082-4 0 00006
2 59743 43.0029 103.9894 0001166 275.3677 84.7042 15.27571732 08
| Epoch (UTC): | 25 May 2026 06:35:12 |
| Eccentricity: | 0.0001166 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.9894° |
| argument of perigee: | 275.3677° |
| revolutions per day: | 15.27571732 |
| mean anomaly at epoch: | 84.7042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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