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 26110.10232422 +.00000000 +00000-0 +14847-3 0 00006
2 39161 97.7345 166.3208 0007880 194.6740 165.4246 14.81221215 02
| Epoch (UTC): | 20 April 2026 02:27:20 |
| Eccentricity: | 0.0007880 |
| inclination: | 97.7345° |
| perigee height: | 620 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 166.3208° |
| argument of perigee: | 194.6740° |
| revolutions per day: | 14.81221215 |
| mean anomaly at epoch: | 165.4246° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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