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 64083U 26145.42636970 +.00000000 +00000-0 +56519-3 0 00008
2 64083 43.0014 128.4096 0001392 272.5340 87.5353 15.27599317 03
| Epoch (UTC): | 25 May 2026 10:13:58 |
| Eccentricity: | 0.0001392 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 128.4096° |
| argument of perigee: | 272.5340° |
| revolutions per day: | 15.27599317 |
| mean anomaly at epoch: | 87.5353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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