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 59156U 26145.39151845 +.00000000 +00000-0 +15795-4 0 00004
2 59156 43.0016 37.5162 0000947 275.4171 84.6573 15.27579032 07
| Epoch (UTC): | 25 May 2026 09:23:47 |
| Eccentricity: | 0.0000947 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 37.5162° |
| argument of perigee: | 275.4171° |
| revolutions per day: | 15.27579032 |
| mean anomaly at epoch: | 84.6573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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