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 43782U 26156.43152264 +.00000000 +00000-0 +38460-3 0 00008
2 43782 97.4061 209.9971 0009492 345.8710 14.2259 15.21654849 00
| Epoch (UTC): | 05 June 2026 10:21:23 |
| Eccentricity: | 0.0009492 |
| inclination: | 97.4061° |
| perigee height: | 494 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 209.9971° |
| argument of perigee: | 345.8710° |
| revolutions per day: | 15.21654849 |
| mean anomaly at epoch: | 14.2259° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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