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 63266U 26145.32597762 +.00000000 +00000-0 +18645-2 0 00001
2 63266 42.9998 10.1792 0000788 7.7731 352.3148 15.70893153 02
| Epoch (UTC): | 25 May 2026 07:49:24 |
| Eccentricity: | 0.0000788 |
| inclination: | 42.9998° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 10.1792° |
| argument of perigee: | 7.7731° |
| revolutions per day: | 15.70893153 |
| mean anomaly at epoch: | 352.3148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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