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 67155U 26145.53638535 +.00000000 +00000-0 +45385-3 0 00001
2 67155 51.8989 90.7839 0001134 73.5465 286.5622 14.79984196 00
| Epoch (UTC): | 25 May 2026 12:52:23 |
| Eccentricity: | 0.0001134 |
| inclination: | 51.8989° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 90.7839° |
| argument of perigee: | 73.5465° |
| revolutions per day: | 14.79984196 |
| mean anomaly at epoch: | 286.5622° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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