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 63286U 26145.53295596 +.00000000 +00000-0 +66476-3 0 00002
2 63286 43.0001 167.9800 0001958 255.8012 104.2623 15.27606387 05
| Epoch (UTC): | 25 May 2026 12:47:27 |
| Eccentricity: | 0.0001958 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 167.9800° |
| argument of perigee: | 255.8012° |
| revolutions per day: | 15.27606387 |
| mean anomaly at epoch: | 104.2623° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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