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 67783U 26145.58335647 +.00000000 +00000-0 +30062-2 0 00006
2 67783 51.8994 212.9880 0008872 357.3928 156.3231 14.87576855 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0008872 |
| inclination: | 51.8994° |
| perigee height: | 599 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 212.9880° |
| argument of perigee: | 357.3928° |
| revolutions per day: | 14.87576855 |
| mean anomaly at epoch: | 156.3231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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