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 63467U 26145.56911206 +.00000000 +00000-0 +14726-3 0 00000
2 63467 43.0007 185.6868 0000843 8.7979 351.2887 15.27576341 04
| Epoch (UTC): | 25 May 2026 13:39:31 |
| Eccentricity: | 0.0000843 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.6868° |
| argument of perigee: | 8.7979° |
| revolutions per day: | 15.27576341 |
| mean anomaly at epoch: | 351.2887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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