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 59128U 26145.37779198 +.00000000 +00000-0 +18909-3 0 00007
2 59128 97.5611 283.5995 0008851 327.9216 32.1486 15.31811790 09
| Epoch (UTC): | 25 May 2026 09:04:01 |
| Eccentricity: | 0.0008851 |
| inclination: | 97.5611° |
| perigee height: | 464 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 283.5995° |
| argument of perigee: | 327.9216° |
| revolutions per day: | 15.31811790 |
| mean anomaly at epoch: | 32.1486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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