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 64337U 26145.12087779 +.00000000 +00000-0 +61440-3 0 00003
2 64337 43.0043 49.7108 0001367 261.0833 98.9864 15.27598092 00
| Epoch (UTC): | 25 May 2026 02:54:03 |
| Eccentricity: | 0.0001367 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 49.7108° |
| argument of perigee: | 261.0833° |
| revolutions per day: | 15.27598092 |
| mean anomaly at epoch: | 98.9864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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