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 00737U 26151.95168713 +.00000000 +00000-0 +00000-0 0 00005
2 00737 46.4723 3.8979 2599075 3.0740 358.2910 7.39534494 08
| Epoch (UTC): | 31 May 2026 22:50:25 |
| Eccentricity: | 0.2599075 |
| inclination: | 46.4723° |
| perigee height: | 1858 km |
| apogee height: | 7643 km |
| right ascension of ascending node: | 3.8979° |
| argument of perigee: | 3.0740° |
| revolutions per day: | 7.39534494 |
| mean anomaly at epoch: | 358.2910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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