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 63964U 26144.90643529 +.00000000 +00000-0 +30433-3 0 00002
2 63964 43.0001 105.7013 0002944 282.4029 77.6493 15.27567727 06
| Epoch (UTC): | 24 May 2026 21:45:16 |
| Eccentricity: | 0.0002944 |
| inclination: | 43.0001° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 105.7013° |
| argument of perigee: | 282.4029° |
| revolutions per day: | 15.27567727 |
| mean anomaly at epoch: | 77.6493° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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