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 64765U 26144.99259778 +.00000000 +00000-0 +54379-3 0 00005
2 64765 53.1601 247.6476 0001069 66.9478 293.1637 15.34402148 01
| Epoch (UTC): | 24 May 2026 23:49:20 |
| Eccentricity: | 0.0001069 |
| inclination: | 53.1601° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 247.6476° |
| argument of perigee: | 66.9478° |
| revolutions per day: | 15.34402148 |
| mean anomaly at epoch: | 293.1637° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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