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 64239U 26144.89694994 +.00000000 +00000-0 +12594-2 0 00005
2 64239 42.9975 109.4483 0000817 166.9740 193.1149 15.70948350 00
| Epoch (UTC): | 24 May 2026 21:31:36 |
| Eccentricity: | 0.0000817 |
| inclination: | 42.9975° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 109.4483° |
| argument of perigee: | 166.9740° |
| revolutions per day: | 15.70948350 |
| mean anomaly at epoch: | 193.1149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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