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 64881U 26145.62859150 +.00000000 +00000-0 +42279-3 0 00001
2 64881 97.4539 114.7204 0004948 248.8649 111.2064 15.32242459 03
| Epoch (UTC): | 25 May 2026 15:05:10 |
| Eccentricity: | 0.0004948 |
| inclination: | 97.4539° |
| perigee height: | 466 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 114.7204° |
| argument of perigee: | 248.8649° |
| revolutions per day: | 15.32242459 |
| mean anomaly at epoch: | 111.2064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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