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 64498U 26145.32195303 +.00000000 +00000-0 +77494-3 0 00002
2 64498 53.1600 120.6635 0001157 85.8006 274.3127 15.30182794 08
| Epoch (UTC): | 25 May 2026 07:43:36 |
| Eccentricity: | 0.0001157 |
| inclination: | 53.1600° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 120.6635° |
| argument of perigee: | 85.8006° |
| revolutions per day: | 15.30182794 |
| mean anomaly at epoch: | 274.3127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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