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 58788U 26145.27068859 +.00000000 +00000-0 -82402-4 0 00003
2 58788 43.0021 93.1392 0001111 247.2078 112.8656 15.27577156 04
| Epoch (UTC): | 25 May 2026 06:29:47 |
| Eccentricity: | 0.0001111 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 93.1392° |
| argument of perigee: | 247.2078° |
| revolutions per day: | 15.27577156 |
| mean anomaly at epoch: | 112.8656° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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