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 64476U 26145.32118800 +.00000000 +00000-0 +75308-3 0 00007
2 64476 53.1601 118.5419 0000943 88.3772 271.7339 15.35410540 05
| Epoch (UTC): | 25 May 2026 07:42:30 |
| Eccentricity: | 0.0000943 |
| inclination: | 53.1601° |
| perigee height: | 459 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 118.5419° |
| argument of perigee: | 88.3772° |
| revolutions per day: | 15.35410540 |
| mean anomaly at epoch: | 271.7339° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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