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 59551U 26145.37404755 +.00000000 +00000-0 -37144-5 0 00006
2 59551 43.0001 270.3243 0000632 275.4202 84.6577 15.27575038 09
| Epoch (UTC): | 25 May 2026 08:58:37 |
| Eccentricity: | 0.0000632 |
| inclination: | 43.0001° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 270.3243° |
| argument of perigee: | 275.4202° |
| revolutions per day: | 15.27575038 |
| mean anomaly at epoch: | 84.6577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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