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 64680U 26145.32999737 +.00000000 +00000-0 +56108-3 0 00007
2 64680 53.1587 129.9476 0000933 103.4006 256.7100 15.34409615 01
| Epoch (UTC): | 25 May 2026 07:55:11 |
| Eccentricity: | 0.0000933 |
| inclination: | 53.1587° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 129.9476° |
| argument of perigee: | 103.4006° |
| revolutions per day: | 15.34409615 |
| mean anomaly at epoch: | 256.7100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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