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 64335U 26145.13501935 +.00000000 +00000-0 +72940-3 0 00004
2 64335 43.0039 49.8160 0001757 255.5598 104.5059 15.27603527 01
| Epoch (UTC): | 25 May 2026 03:14:25 |
| Eccentricity: | 0.0001757 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 49.8160° |
| argument of perigee: | 255.5598° |
| revolutions per day: | 15.27603527 |
| mean anomaly at epoch: | 104.5059° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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