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 39161U 26073.89235891 +.00000000 +00000-0 +28846-3 0 00007
2 39161 97.7414 131.3589 0007296 331.9958 28.0862 14.81093565 04
| Epoch (UTC): | 14 March 2026 21:24:59 |
| Eccentricity: | 0.0007296 |
| inclination: | 97.7414° |
| perigee height: | 621 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 131.3589° |
| argument of perigee: | 331.9958° |
| revolutions per day: | 14.81093565 |
| mean anomaly at epoch: | 28.0862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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