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 64938U 26145.39998117 +.00000000 +00000-0 +38402-3 0 00008
2 64938 97.4479 9.3847 0002476 68.6627 291.4864 15.05651981 02
| Epoch (UTC): | 25 May 2026 09:35:58 |
| Eccentricity: | 0.0002476 |
| inclination: | 97.4479° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 9.3847° |
| argument of perigee: | 68.6627° |
| revolutions per day: | 15.05651981 |
| mean anomaly at epoch: | 291.4864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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