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 59577U 26145.43401123 +.00000000 +00000-0 +72619-3 0 00000
2 59577 43.0020 295.2233 0005166 308.6307 51.4083 15.30348037 00
| Epoch (UTC): | 25 May 2026 10:24:58 |
| Eccentricity: | 0.0005166 |
| inclination: | 43.0020° |
| perigee height: | 471 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 295.2233° |
| argument of perigee: | 308.6307° |
| revolutions per day: | 15.30348037 |
| mean anomaly at epoch: | 51.4083° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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