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 58630U 26145.61061458 +.00000000 +00000-0 -10155-3 0 00000
2 58630 43.0013 356.2795 0001176 283.6326 76.4395 15.27561166 01
| Epoch (UTC): | 25 May 2026 14:39:17 |
| Eccentricity: | 0.0001176 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 356.2795° |
| argument of perigee: | 283.6326° |
| revolutions per day: | 15.27561166 |
| mean anomaly at epoch: | 76.4395° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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