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 26145.38148758 +.00000000 +00000-0 +98691-4 0 00006
2 38337 98.2015 86.2841 0001779 91.7982 19.8655 14.57099119 00
| Epoch (UTC): | 25 May 2026 09:09:20 |
| Eccentricity: | 0.0001779 |
| inclination: | 98.2015° |
| perigee height: | 701 km |
| apogee height: | 704 km |
| right ascension of ascending node: | 86.2841° |
| argument of perigee: | 91.7982° |
| revolutions per day: | 14.57099119 |
| mean anomaly at epoch: | 19.8655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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