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 67191U 26145.54102684 +.00000000 +00000-0 +49284-3 0 00005
2 67191 42.9932 237.1127 0001518 268.3130 91.7547 15.27583472 03
| Epoch (UTC): | 25 May 2026 12:59:04 |
| Eccentricity: | 0.0001518 |
| inclination: | 42.9932° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 237.1127° |
| argument of perigee: | 268.3130° |
| revolutions per day: | 15.27583472 |
| mean anomaly at epoch: | 91.7547° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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