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 63472U 26145.59223296 +.00000000 +00000-0 +50146-3 0 00000
2 63472 42.9994 185.8437 0001316 277.9060 82.1642 15.27596646 03
| Epoch (UTC): | 25 May 2026 14:12:48 |
| Eccentricity: | 0.0001316 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.8437° |
| argument of perigee: | 277.9060° |
| revolutions per day: | 15.27596646 |
| mean anomaly at epoch: | 82.1642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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