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 64383U 26145.33335647 +.00000000 +00000-0 +22760-2 0 00008
2 64383 43.0001 107.3287 0001053 273.4272 109.9275 15.27545705 02
| Epoch (UTC): | 25 May 2026 08:00:01 |
| Eccentricity: | 0.0001053 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 107.3287° |
| argument of perigee: | 273.4272° |
| revolutions per day: | 15.27545705 |
| mean anomaly at epoch: | 109.9275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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