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 58789U 26145.55778038 +.00000000 +00000-0 +41282-4 0 00002
2 58789 43.0034 90.9929 0000692 270.9001 89.1772 15.27569657 04
| Epoch (UTC): | 25 May 2026 13:23:12 |
| Eccentricity: | 0.0000692 |
| inclination: | 43.0034° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 90.9929° |
| argument of perigee: | 270.9001° |
| revolutions per day: | 15.27569657 |
| mean anomaly at epoch: | 89.1772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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