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 57786U 26145.40927558 +.00000000 +00000-0 +36584-4 0 00004
2 57786 43.0021 120.9071 0001365 265.9898 94.0798 15.27579450 09
| Epoch (UTC): | 25 May 2026 09:49:21 |
| Eccentricity: | 0.0001365 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 120.9071° |
| argument of perigee: | 265.9898° |
| revolutions per day: | 15.27579450 |
| mean anomaly at epoch: | 94.0798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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