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 26145.58853654 +.00000000 +00000-0 +11989-3 0 00009
2 32783 97.7648 195.0677 0011650 177.7277 182.3990 14.79201466 04
| Epoch (UTC): | 25 May 2026 14:07:29 |
| Eccentricity: | 0.0011650 |
| inclination: | 97.7648° |
| perigee height: | 624 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 195.0677° |
| argument of perigee: | 177.7277° |
| revolutions per day: | 14.79201466 |
| mean anomaly at epoch: | 182.3990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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