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 67183U 26145.55372740 +.00000000 +00000-0 +45742-3 0 00004
2 67183 43.0013 236.3525 0000735 278.7655 81.3113 15.27592108 06
| Epoch (UTC): | 25 May 2026 13:17:22 |
| Eccentricity: | 0.0000735 |
| inclination: | 43.0013° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.3525° |
| argument of perigee: | 278.7655° |
| revolutions per day: | 15.27592108 |
| mean anomaly at epoch: | 81.3113° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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