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 26109.56189757 +.00000000 +00000-0 +14553-3 0 00000
2 39161 97.7346 165.7992 0007839 196.4237 163.6723 14.81219983 00
| Epoch (UTC): | 19 April 2026 13:29:07 |
| Eccentricity: | 0.0007839 |
| inclination: | 97.7346° |
| perigee height: | 620 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 165.7992° |
| argument of perigee: | 196.4237° |
| revolutions per day: | 14.81219983 |
| mean anomaly at epoch: | 163.6723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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