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 64005U 26145.43375873 +.00000000 +00000-0 +67663-3 0 00007
2 64005 42.9998 284.4350 0001121 284.4557 75.6171 15.27593407 04
| Epoch (UTC): | 25 May 2026 10:24:36 |
| Eccentricity: | 0.0001121 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 284.4350° |
| argument of perigee: | 284.4557° |
| revolutions per day: | 15.27593407 |
| mean anomaly at epoch: | 75.6171° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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