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 67151U 26145.03256861 +.00000000 +00000-0 +43469-3 0 00001
2 67151 51.8995 90.5206 0000917 70.3864 289.7198 14.79960331 03
| Epoch (UTC): | 25 May 2026 00:46:53 |
| Eccentricity: | 0.0000917 |
| inclination: | 51.8995° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 90.5206° |
| argument of perigee: | 70.3864° |
| revolutions per day: | 14.79960331 |
| mean anomaly at epoch: | 289.7198° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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