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 64489U 26145.34836221 +.00000000 +00000-0 +19591-2 0 00008
2 64489 53.1575 120.8361 0001314 104.1492 255.9655 15.30229341 07
| Epoch (UTC): | 25 May 2026 08:21:38 |
| Eccentricity: | 0.0001314 |
| inclination: | 53.1575° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 120.8361° |
| argument of perigee: | 104.1492° |
| revolutions per day: | 15.30229341 |
| mean anomaly at epoch: | 255.9655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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