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 64108U 26145.09421698 +.00000000 +00000-0 +39493-3 0 00000
2 64108 53.1602 31.6373 0001088 79.6853 280.4271 15.31715353 04
| Epoch (UTC): | 25 May 2026 02:15:40 |
| Eccentricity: | 0.0001088 |
| inclination: | 53.1602° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 31.6373° |
| argument of perigee: | 79.6853° |
| revolutions per day: | 15.31715353 |
| mean anomaly at epoch: | 280.4271° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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