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 35756U 26151.74602203 +.00000000 +00000-0 +00000-0 0 00008
2 35756 0.8587 270.2109 0003525 162.6224 241.1156 1.00270947 05
| Epoch (UTC): | 31 May 2026 17:54:16 |
| Eccentricity: | 0.0003525 |
| inclination: | 0.8587° |
| perigee height: | 35772 km |
| apogee height: | 35802 km |
| right ascension of ascending node: | 270.2109° |
| argument of perigee: | 162.6224° |
| revolutions per day: | 1.00270947 |
| mean anomaly at epoch: | 241.1156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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