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 64480U 26145.31985252 +.00000000 +00000-0 +89872-3 0 00005
2 64480 53.1603 120.6597 0001235 80.6149 279.4991 15.30203930 08
| Epoch (UTC): | 25 May 2026 07:40:35 |
| Eccentricity: | 0.0001235 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 120.6597° |
| argument of perigee: | 80.6149° |
| revolutions per day: | 15.30203930 |
| mean anomaly at epoch: | 279.4991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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