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 64766U 26145.54409661 +.00000000 +00000-0 +63970-3 0 00003
2 64766 53.1603 246.1149 0000588 41.7046 318.4000 15.30198979 07
| Epoch (UTC): | 25 May 2026 13:03:29 |
| Eccentricity: | 0.0000588 |
| inclination: | 53.1603° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 246.1149° |
| argument of perigee: | 41.7046° |
| revolutions per day: | 15.30198979 |
| mean anomaly at epoch: | 318.4000° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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