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 59167U 26145.37401318 +.00000000 +00000-0 +40013-4 0 00008
2 59167 43.0022 33.9380 0000954 269.7129 90.3613 15.27583096 09
| Epoch (UTC): | 25 May 2026 08:58:34 |
| Eccentricity: | 0.0000954 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.9380° |
| argument of perigee: | 269.7129° |
| revolutions per day: | 15.27583096 |
| mean anomaly at epoch: | 90.3613° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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