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 58509U 26145.40554589 +.00000000 +00000-0 +89352-3 0 00008
2 58509 43.0041 37.0285 0001467 261.0623 99.0062 15.27570093 09
| Epoch (UTC): | 25 May 2026 09:43:59 |
| Eccentricity: | 0.0001467 |
| inclination: | 43.0041° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 37.0285° |
| argument of perigee: | 261.0623° |
| revolutions per day: | 15.27570093 |
| mean anomaly at epoch: | 99.0062° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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