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 64764U 26145.56199068 +.00000000 +00000-0 +39866-3 0 00007
2 64764 53.1591 244.8085 0000762 60.2156 299.8922 15.34383351 06
| Epoch (UTC): | 25 May 2026 13:29:15 |
| Eccentricity: | 0.0000762 |
| inclination: | 53.1591° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 244.8085° |
| argument of perigee: | 60.2156° |
| revolutions per day: | 15.34383351 |
| mean anomaly at epoch: | 299.8922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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