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 67791U 26145.51079826 +.00000000 +00000-0 +76103-3 0 00009
2 67791 51.8814 208.9766 0011307 335.5260 24.5188 15.36089782 00
| Epoch (UTC): | 25 May 2026 12:15:32 |
| Eccentricity: | 0.0011307 |
| inclination: | 51.8814° |
| perigee height: | 450 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 208.9766° |
| argument of perigee: | 335.5260° |
| revolutions per day: | 15.36089782 |
| mean anomaly at epoch: | 24.5188° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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