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 58749U 26145.47667656 +.00000000 +00000-0 -21010-4 0 00000
2 58749 43.0024 146.3452 0001560 267.4670 92.6003 15.27583373 01
| Epoch (UTC): | 25 May 2026 11:26:24 |
| Eccentricity: | 0.0001560 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 146.3452° |
| argument of perigee: | 267.4670° |
| revolutions per day: | 15.27583373 |
| mean anomaly at epoch: | 92.6003° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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