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 64736U 26145.50915666 +.00000000 +00000-0 +41277-3 0 00009
2 64736 53.1588 184.1959 0000986 66.9981 293.1123 15.30207127 06
| Epoch (UTC): | 25 May 2026 12:13:11 |
| Eccentricity: | 0.0000986 |
| inclination: | 53.1588° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.1959° |
| argument of perigee: | 66.9981° |
| revolutions per day: | 15.30207127 |
| mean anomaly at epoch: | 293.1123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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