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 64139U 26145.31092435 +.00000000 +00000-0 +12858-3 0 00008
2 64139 43.0029 4.9755 0001067 288.4777 71.5959 15.27588929 02
| Epoch (UTC): | 25 May 2026 07:27:43 |
| Eccentricity: | 0.0001067 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 4.9755° |
| argument of perigee: | 288.4777° |
| revolutions per day: | 15.27588929 |
| mean anomaly at epoch: | 71.5959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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