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 57756U 26145.40696419 +.00000000 +00000-0 +93613-4 0 00006
2 57756 81.0037 28.0714 0010805 58.6511 301.5702 13.86352658 08
| Epoch (UTC): | 25 May 2026 09:46:01 |
| Eccentricity: | 0.0010805 |
| inclination: | 81.0037° |
| perigee height: | 934 km |
| apogee height: | 949 km |
| right ascension of ascending node: | 28.0714° |
| argument of perigee: | 58.6511° |
| revolutions per day: | 13.86352658 |
| mean anomaly at epoch: | 301.5702° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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