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 64890U 26145.62552698 +.00000000 +00000-0 +34100-3 0 00002
2 64890 97.4536 114.3727 0005135 232.4566 127.6209 15.30488478 05
| Epoch (UTC): | 25 May 2026 15:00:45 |
| Eccentricity: | 0.0005135 |
| inclination: | 97.4536° |
| perigee height: | 471 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 114.3727° |
| argument of perigee: | 232.4566° |
| revolutions per day: | 15.30488478 |
| mean anomaly at epoch: | 127.6209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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