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 57758U 26145.43461601 +.00000000 +00000-0 +10109-3 0 00002
2 57758 80.9984 27.8632 0009508 58.0748 302.1333 13.86268719 00
| Epoch (UTC): | 25 May 2026 10:25:50 |
| Eccentricity: | 0.0009508 |
| inclination: | 80.9984° |
| perigee height: | 935 km |
| apogee height: | 949 km |
| right ascension of ascending node: | 27.8632° |
| argument of perigee: | 58.0748° |
| revolutions per day: | 13.86268719 |
| mean anomaly at epoch: | 302.1333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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