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 64483U 26145.23554990 +.00000000 +00000-0 +45985-3 0 00007
2 64483 53.1574 120.8441 0001230 93.0153 267.0988 15.30166373 04
| Epoch (UTC): | 25 May 2026 05:39:11 |
| Eccentricity: | 0.0001230 |
| inclination: | 53.1574° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 120.8441° |
| argument of perigee: | 93.0153° |
| revolutions per day: | 15.30166373 |
| mean anomaly at epoch: | 267.0988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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