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 63066U 26145.52412392 +.00000000 +00000-0 +57049-3 0 00008
2 63066 43.0061 72.8850 0002887 265.9229 94.1293 15.27587807 05
| Epoch (UTC): | 25 May 2026 12:34:44 |
| Eccentricity: | 0.0002887 |
| inclination: | 43.0061° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 72.8850° |
| argument of perigee: | 265.9229° |
| revolutions per day: | 15.27587807 |
| mean anomaly at epoch: | 94.1293° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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