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 66763U 26145.46179259 +.00000000 +00000-0 +15970-3 0 00007
2 66763 97.4206 218.5547 0013475 78.3815 281.8927 15.11470150 04
| Epoch (UTC): | 25 May 2026 11:04:58 |
| Eccentricity: | 0.0013475 |
| inclination: | 97.4206° |
| perigee height: | 522 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 218.5547° |
| argument of perigee: | 78.3815° |
| revolutions per day: | 15.11470150 |
| mean anomaly at epoch: | 281.8927° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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