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 58626U 26145.30843811 +.00000000 +00000-0 +28373-4 0 00003
2 58626 43.0046 354.0164 0001850 279.0054 81.0588 15.27576907 09
| Epoch (UTC): | 25 May 2026 07:24:09 |
| Eccentricity: | 0.0001850 |
| inclination: | 43.0046° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 354.0164° |
| argument of perigee: | 279.0054° |
| revolutions per day: | 15.27576907 |
| mean anomaly at epoch: | 81.0588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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