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 64140U 26145.64814887 +.00000000 +00000-0 +57113-3 0 00002
2 64140 42.9998 3.2077 0000744 238.8522 121.2257 15.27586700 03
| Epoch (UTC): | 25 May 2026 15:33:20 |
| Eccentricity: | 0.0000744 |
| inclination: | 42.9998° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 3.2077° |
| argument of perigee: | 238.8522° |
| revolutions per day: | 15.27586700 |
| mean anomaly at epoch: | 121.2257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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