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 59746U 26145.34368443 +.00000000 +00000-0 +47982-4 0 00001
2 59746 43.0035 103.6476 0001321 267.1037 92.9663 15.27575398 05
| Epoch (UTC): | 25 May 2026 08:14:54 |
| Eccentricity: | 0.0001321 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.6476° |
| argument of perigee: | 267.1037° |
| revolutions per day: | 15.27575398 |
| mean anomaly at epoch: | 92.9663° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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