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 32783U 26114.20072145 +.00000000 +00000-0 +12053-4 0 00006
2 32783 97.7681 164.7408 0010403 290.3853 69.6241 14.79167493 00
| Epoch (UTC): | 24 April 2026 04:49:02 |
| Eccentricity: | 0.0010403 |
| inclination: | 97.7681° |
| perigee height: | 625 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 164.7408° |
| argument of perigee: | 290.3853° |
| revolutions per day: | 14.79167493 |
| mean anomaly at epoch: | 69.6241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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