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 67851U 26145.38017174 +.00000000 +00000-0 +25083-3 0 00000
2 67851 53.1588 208.3122 0001109 79.0016 281.1109 15.30200094 07
| Epoch (UTC): | 25 May 2026 09:07:26 |
| Eccentricity: | 0.0001109 |
| inclination: | 53.1588° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 208.3122° |
| argument of perigee: | 79.0016° |
| revolutions per day: | 15.30200094 |
| mean anomaly at epoch: | 281.1109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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