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 64825U 26145.17547719 +.00000000 +00000-0 +37938-3 0 00000
2 64825 51.9017 317.3713 0000694 120.9588 239.1443 14.79938914 08
| Epoch (UTC): | 25 May 2026 04:12:41 |
| Eccentricity: | 0.0000694 |
| inclination: | 51.9017° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 317.3713° |
| argument of perigee: | 120.9588° |
| revolutions per day: | 14.79938914 |
| mean anomaly at epoch: | 239.1443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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