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 39086U 26136.82650948 +.00000000 +00000-0 +33863-4 0 00006
2 39086 98.5559 323.7909 0002457 45.4543 314.6841 14.32847777 02
| Epoch (UTC): | 16 May 2026 19:50:10 |
| Eccentricity: | 0.0002457 |
| inclination: | 98.5559° |
| perigee height: | 780 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 323.7909° |
| argument of perigee: | 45.4543° |
| revolutions per day: | 14.32847777 |
| mean anomaly at epoch: | 314.6841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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