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 51626U 26145.37062083 +.00000000 +00000-0 +28260-3 0 00001
2 51626 87.9160 10.3942 0001651 63.2549 296.8751 13.17649302 08
| Epoch (UTC): | 25 May 2026 08:53:41 |
| Eccentricity: | 0.0001651 |
| inclination: | 87.9160° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3942° |
| argument of perigee: | 63.2549° |
| revolutions per day: | 13.17649302 |
| mean anomaly at epoch: | 296.8751° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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