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 43784U 26111.63961601 +.00000000 +00000-0 +39270-3 0 00006
2 43784 97.3916 166.5151 0004521 120.1208 240.0479 15.25917983 00
| Epoch (UTC): | 21 April 2026 15:21:02 |
| Eccentricity: | 0.0004521 |
| inclination: | 97.3916° |
| perigee height: | 485 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 166.5151° |
| argument of perigee: | 120.1208° |
| revolutions per day: | 15.25917983 |
| mean anomaly at epoch: | 240.0479° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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