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 64333U 26145.41840726 +.00000000 +00000-0 +55911-3 0 00006
2 64333 42.9968 48.5125 0000451 293.4050 66.6754 15.27587282 08
| Epoch (UTC): | 25 May 2026 10:02:30 |
| Eccentricity: | 0.0000451 |
| inclination: | 42.9968° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 48.5125° |
| argument of perigee: | 293.4050° |
| revolutions per day: | 15.27587282 |
| mean anomaly at epoch: | 66.6754° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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