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 67555U 26145.61430441 +.00000000 +00000-0 +60098-3 0 00008
2 67555 97.2871 32.6741 0001928 92.8298 267.3165 15.33465142 09
| Epoch (UTC): | 25 May 2026 14:44:35 |
| Eccentricity: | 0.0001928 |
| inclination: | 97.2871° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 32.6741° |
| argument of perigee: | 92.8298° |
| revolutions per day: | 15.33465142 |
| mean anomaly at epoch: | 267.3165° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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