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 63783U 26145.59366169 +.00000000 +00000-0 +71228-3 0 00006
2 63783 43.0033 338.2195 0001777 275.7654 84.2995 15.27593528 05
| Epoch (UTC): | 25 May 2026 14:14:52 |
| Eccentricity: | 0.0001777 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.2195° |
| argument of perigee: | 275.7654° |
| revolutions per day: | 15.27593528 |
| mean anomaly at epoch: | 84.2995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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