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 63425U 26145.41633331 +.00000000 +00000-0 +68468-3 0 00000
2 63425 43.0036 33.7483 0001959 271.3674 88.6953 15.27593064 01
| Epoch (UTC): | 25 May 2026 09:59:31 |
| Eccentricity: | 0.0001959 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.7483° |
| argument of perigee: | 271.3674° |
| revolutions per day: | 15.27593064 |
| mean anomaly at epoch: | 88.6953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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