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 56843U 26145.41243661 +.00000000 +00000-0 +11333-3 0 00008
2 56843 43.0060 33.5249 0001291 272.9182 87.1522 15.27585944 06
| Epoch (UTC): | 25 May 2026 09:53:54 |
| Eccentricity: | 0.0001291 |
| inclination: | 43.0060° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.5249° |
| argument of perigee: | 272.9182° |
| revolutions per day: | 15.27585944 |
| mean anomaly at epoch: | 87.1522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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