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 64149U 26145.57781014 +.00000000 +00000-0 +14364-3 0 00009
2 64149 97.4493 196.8671 0001594 135.2030 224.9326 15.05654696 08
| Epoch (UTC): | 25 May 2026 13:52:02 |
| Eccentricity: | 0.0001594 |
| inclination: | 97.4493° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 196.8671° |
| argument of perigee: | 135.2030° |
| revolutions per day: | 15.05654696 |
| mean anomaly at epoch: | 224.9326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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