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 26073.62212289 +.00000000 +00000-0 +29936-3 0 00005
2 39161 97.7415 131.0979 0007331 332.9946 27.0885 14.81092785 00
| Epoch (UTC): | 14 March 2026 14:55:51 |
| Eccentricity: | 0.0007331 |
| inclination: | 97.7415° |
| perigee height: | 621 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 131.0979° |
| argument of perigee: | 332.9946° |
| revolutions per day: | 14.81092785 |
| mean anomaly at epoch: | 27.0885° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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