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 64682U 26145.25349860 +.00000000 +00000-0 +98290-3 0 00005
2 64682 53.1605 120.9464 0000957 85.5510 274.5600 15.30218850 06
| Epoch (UTC): | 25 May 2026 06:05:02 |
| Eccentricity: | 0.0000957 |
| inclination: | 53.1605° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 120.9464° |
| argument of perigee: | 85.5510° |
| revolutions per day: | 15.30218850 |
| mean anomaly at epoch: | 274.5600° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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