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 67153U 26145.58335647 +.00000000 +00000-0 -21526-3 0 00004
2 67153 51.8988 59.9439 0001068 52.6461 234.8853 14.80906589 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001068 |
| inclination: | 51.8988° |
| perigee height: | 626 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 59.9439° |
| argument of perigee: | 52.6461° |
| revolutions per day: | 14.80906589 |
| mean anomaly at epoch: | 234.8853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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