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 46576U 26145.58335647 +.00000000 +00000-0 +84567-3 0 00003
2 46576 53.0262 100.6691 0007698 69.1190 131.5566 15.88276679 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0007698 |
| inclination: | 53.0262° |
| perigee height: | 302 km |
| apogee height: | 312 km |
| right ascension of ascending node: | 100.6691° |
| argument of perigee: | 69.1190° |
| revolutions per day: | 15.88276679 |
| mean anomaly at epoch: | 131.5566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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