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 58671U 26145.32034728 +.00000000 +00000-0 +40228-4 0 00007
2 58671 43.0020 12.5655 0001235 276.4526 83.6185 15.27578957 02
| Epoch (UTC): | 25 May 2026 07:41:18 |
| Eccentricity: | 0.0001235 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 12.5655° |
| argument of perigee: | 276.4526° |
| revolutions per day: | 15.27578957 |
| mean anomaly at epoch: | 83.6185° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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