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 67787U 26145.58335647 +.00000000 +00000-0 +40747-2 0 00001
2 67787 51.9002 215.2005 0002075 126.7195 103.9664 14.76374574 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0002075 |
| inclination: | 51.9002° |
| perigee height: | 639 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 215.2005° |
| argument of perigee: | 126.7195° |
| revolutions per day: | 14.76374574 |
| mean anomaly at epoch: | 103.9664° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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