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 43576U 26145.51243573 +.00000000 +00000-0 +48829-5 0 00002
2 43576 86.3967 66.2086 0002280 80.1327 280.0126 14.34217912 00
| Epoch (UTC): | 25 May 2026 12:17:54 |
| Eccentricity: | 0.0002280 |
| inclination: | 86.3967° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 66.2086° |
| argument of perigee: | 80.1327° |
| revolutions per day: | 14.34217912 |
| mean anomaly at epoch: | 280.0126° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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