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 64817U 26145.50222403 +.00000000 +00000-0 +46007-3 0 00005
2 64817 51.8999 325.8906 0000785 126.1052 233.9983 14.79977986 03
| Epoch (UTC): | 25 May 2026 12:03:12 |
| Eccentricity: | 0.0000785 |
| inclination: | 51.8999° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 325.8906° |
| argument of perigee: | 126.1052° |
| revolutions per day: | 14.79977986 |
| mean anomaly at epoch: | 233.9983° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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