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 67591U 26145.44792153 +.00000000 +00000-0 +66971-3 0 00006
2 67591 97.2856 210.5137 0000731 102.2131 257.9194 15.33451205 03
| Epoch (UTC): | 25 May 2026 10:45:00 |
| Eccentricity: | 0.0000731 |
| inclination: | 97.2856° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 210.5137° |
| argument of perigee: | 102.2131° |
| revolutions per day: | 15.33451205 |
| mean anomaly at epoch: | 257.9194° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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