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 59631U 26145.50451141 +.00000000 +00000-0 +46331-4 0 00007
2 59631 43.0045 65.6674 0001180 259.0850 100.9869 15.27576303 07
| Epoch (UTC): | 25 May 2026 12:06:29 |
| Eccentricity: | 0.0001180 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 65.6674° |
| argument of perigee: | 259.0850° |
| revolutions per day: | 15.27576303 |
| mean anomaly at epoch: | 100.9869° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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