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 39640U 26032.43027205 +.00000000 +00000-0 +16998-3 0 00007
2 39640 65.0100 25.5144 0015478 280.9064 79.0280 14.34156347 05
| Epoch (UTC): | 01 February 2026 10:19:35 |
| Eccentricity: | 0.0015478 |
| inclination: | 65.0100° |
| perigee height: | 767 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 25.5144° |
| argument of perigee: | 280.9064° |
| revolutions per day: | 14.34156347 |
| mean anomaly at epoch: | 79.0280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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