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 64614U 26145.56438936 +.00000000 +00000-0 +57092-3 0 00002
2 64614 53.1610 338.2368 0001250 102.6529 257.4612 15.30207250 07
| Epoch (UTC): | 25 May 2026 13:32:43 |
| Eccentricity: | 0.0001250 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.2368° |
| argument of perigee: | 102.6529° |
| revolutions per day: | 15.30207250 |
| mean anomaly at epoch: | 257.4612° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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