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 39163U 26145.58511512 +.00000000 +00000-0 +00000-0 0 00001
2 39163 0.0747 19.2671 0005422 12.4109 69.1190 1.00271620 03
| Epoch (UTC): | 25 May 2026 14:02:33 |
| Eccentricity: | 0.0005422 |
| inclination: | 0.0747° |
| perigee height: | 35764 km |
| apogee height: | 35810 km |
| right ascension of ascending node: | 19.2671° |
| argument of perigee: | 12.4109° |
| revolutions per day: | 1.00271620 |
| mean anomaly at epoch: | 69.1190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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