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 67184U 26145.54344822 +.00000000 +00000-0 +39117-3 0 00003
2 67184 43.0004 236.2748 0001415 269.6725 90.3965 15.27590884 00
| Epoch (UTC): | 25 May 2026 13:02:33 |
| Eccentricity: | 0.0001415 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.2748° |
| argument of perigee: | 269.6725° |
| revolutions per day: | 15.27590884 |
| mean anomaly at epoch: | 90.3965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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