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 58611U 26145.54839547 +.00000000 +00000-0 +13139-3 0 00007
2 58611 43.0030 94.9342 0001206 253.8872 106.1848 15.27578226 01
| Epoch (UTC): | 25 May 2026 13:09:41 |
| Eccentricity: | 0.0001206 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 94.9342° |
| argument of perigee: | 253.8872° |
| revolutions per day: | 15.27578226 |
| mean anomaly at epoch: | 106.1848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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