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 59769U 26145.37706866 +.00000000 +00000-0 +18143-4 0 00001
2 59769 53.1607 30.8178 0001143 101.6325 258.4805 15.30196293 05
| Epoch (UTC): | 25 May 2026 09:02:58 |
| Eccentricity: | 0.0001143 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 30.8178° |
| argument of perigee: | 101.6325° |
| revolutions per day: | 15.30196293 |
| mean anomaly at epoch: | 258.4805° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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