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 56792U 26145.44470001 +.00000000 +00000-0 -43543-4 0 00004
2 56792 69.9987 151.0809 0003761 270.3071 89.7657 14.98334673 00
| Epoch (UTC): | 25 May 2026 10:40:22 |
| Eccentricity: | 0.0003761 |
| inclination: | 69.9987° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 151.0809° |
| argument of perigee: | 270.3071° |
| revolutions per day: | 14.98334673 |
| mean anomaly at epoch: | 89.7657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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