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 38337U 26160.42003381 +.00000000 +00000-0 +10275-3 0 00001
2 38337 98.2020 101.0934 0001856 80.5804 30.4831 14.57117341 03
| Epoch (UTC): | 09 June 2026 10:04:50 |
| Eccentricity: | 0.0001856 |
| inclination: | 98.2020° |
| perigee height: | 701 km |
| apogee height: | 704 km |
| right ascension of ascending node: | 101.0934° |
| argument of perigee: | 80.5804° |
| revolutions per day: | 14.57117341 |
| mean anomaly at epoch: | 30.4831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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