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 64686U 26145.22918463 +.00000000 +00000-0 +40246-3 0 00005
2 64686 53.1592 130.7389 0000285 32.5787 327.5233 15.34397336 04
| Epoch (UTC): | 25 May 2026 05:30:01 |
| Eccentricity: | 0.0000285 |
| inclination: | 53.1592° |
| perigee height: | 463 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 130.7389° |
| argument of perigee: | 32.5787° |
| revolutions per day: | 15.34397336 |
| mean anomaly at epoch: | 327.5233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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