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 65782U 26145.03655361 +.00000000 +00000-0 +19406-3 0 00001
2 65782 51.9024 55.5058 0000897 93.7021 266.4044 14.79936748 09
| Epoch (UTC): | 25 May 2026 00:52:38 |
| Eccentricity: | 0.0000897 |
| inclination: | 51.9024° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 55.5058° |
| argument of perigee: | 93.7021° |
| revolutions per day: | 14.79936748 |
| mean anomaly at epoch: | 266.4044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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