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 59541U 26145.34963352 +.00000000 +00000-0 +40957-4 0 00009
2 59541 43.0024 270.1477 0001635 267.3602 92.7063 15.27573391 08
| Epoch (UTC): | 25 May 2026 08:23:28 |
| Eccentricity: | 0.0001635 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.1477° |
| argument of perigee: | 267.3602° |
| revolutions per day: | 15.27573391 |
| mean anomaly at epoch: | 92.7063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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