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 64891U 26145.62229005 +.00000000 +00000-0 +42346-3 0 00007
2 64891 97.4531 114.8429 0003802 257.0571 103.0247 15.32561804 00
| Epoch (UTC): | 25 May 2026 14:56:05 |
| Eccentricity: | 0.0003802 |
| inclination: | 97.4531° |
| perigee height: | 466 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 114.8429° |
| argument of perigee: | 257.0571° |
| revolutions per day: | 15.32561804 |
| mean anomaly at epoch: | 103.0247° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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