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 59876U 26145.45404490 +.00000000 +00000-0 +46717-4 0 00005
2 59876 43.0001 204.6944 0001301 278.0713 81.9991 15.27585323 05
| Epoch (UTC): | 25 May 2026 10:53:49 |
| Eccentricity: | 0.0001301 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.6944° |
| argument of perigee: | 278.0713° |
| revolutions per day: | 15.27585323 |
| mean anomaly at epoch: | 81.9991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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