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 65783U 26145.03114697 +.00000000 +00000-0 +45599-3 0 00006
2 65783 51.8995 60.4986 0000795 99.3873 260.7179 14.79924222 05
| Epoch (UTC): | 25 May 2026 00:44:51 |
| Eccentricity: | 0.0000795 |
| inclination: | 51.8995° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 60.4986° |
| argument of perigee: | 99.3873° |
| revolutions per day: | 14.79924222 |
| mean anomaly at epoch: | 260.7179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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