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 64535U 26145.26323140 +.00000000 +00000-0 +25713-3 0 00006
2 64535 97.4647 260.4635 0003124 250.0479 110.0420 15.22170438 06
| Epoch (UTC): | 25 May 2026 06:19:03 |
| Eccentricity: | 0.0003124 |
| inclination: | 97.4647° |
| perigee height: | 497 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 260.4635° |
| argument of perigee: | 250.0479° |
| revolutions per day: | 15.22170438 |
| mean anomaly at epoch: | 110.0420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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