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 63417U 26145.40990669 +.00000000 +00000-0 +64942-3 0 00003
2 63417 43.0065 33.7026 0001658 270.0409 90.0252 15.27599592 06
| Epoch (UTC): | 25 May 2026 09:50:15 |
| Eccentricity: | 0.0001658 |
| inclination: | 43.0065° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.7026° |
| argument of perigee: | 270.0409° |
| revolutions per day: | 15.27599592 |
| mean anomaly at epoch: | 90.0252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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