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 58638U 26145.61367490 +.00000000 +00000-0 +15128-4 0 00008
2 58638 43.0031 352.8652 0001027 270.0173 90.0561 15.27577940 02
| Epoch (UTC): | 25 May 2026 14:43:41 |
| Eccentricity: | 0.0001027 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 352.8652° |
| argument of perigee: | 270.0173° |
| revolutions per day: | 15.27577940 |
| mean anomaly at epoch: | 90.0561° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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