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 58798U 26145.23984001 +.00000000 +00000-0 +12049-3 0 00004
2 58798 43.0034 92.9032 0001201 282.8437 77.2281 15.27580371 02
| Epoch (UTC): | 25 May 2026 05:45:22 |
| Eccentricity: | 0.0001201 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 92.9032° |
| argument of perigee: | 282.8437° |
| revolutions per day: | 15.27580371 |
| mean anomaly at epoch: | 77.2281° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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