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 63775U 26145.51670631 +.00000000 +00000-0 +55934-3 0 00007
2 63775 43.0013 338.4979 0000322 293.7869 66.2949 15.27599102 02
| Epoch (UTC): | 25 May 2026 12:24:03 |
| Eccentricity: | 0.0000322 |
| inclination: | 43.0013° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 338.4979° |
| argument of perigee: | 293.7869° |
| revolutions per day: | 15.27599102 |
| mean anomaly at epoch: | 66.2949° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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