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 59556U 26144.74587843 +.00000000 +00000-0 +51205-4 0 00003
2 59556 43.0020 274.2140 0001569 284.3508 75.7169 15.27580613 05
| Epoch (UTC): | 24 May 2026 17:54:03 |
| Eccentricity: | 0.0001569 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 274.2140° |
| argument of perigee: | 284.3508° |
| revolutions per day: | 15.27580613 |
| mean anomaly at epoch: | 75.7169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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