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 64482U 26145.63378575 +.00000000 +00000-0 +51419-3 0 00002
2 64482 53.1577 119.0623 0001849 78.7563 281.3645 15.30198163 00
| Epoch (UTC): | 25 May 2026 15:12:39 |
| Eccentricity: | 0.0001849 |
| inclination: | 53.1577° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 119.0623° |
| argument of perigee: | 78.7563° |
| revolutions per day: | 15.30198163 |
| mean anomaly at epoch: | 281.3645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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