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 37839U 26018.65864332 +.00000000 +00000-0 +86247-4 0 00008
2 37839 19.9599 136.8282 0018421 225.0383 162.9414 14.13713874 09
| Epoch (UTC): | 18 January 2026 15:48:26 |
| Eccentricity: | 0.0018421 |
| inclination: | 19.9599° |
| perigee height: | 833 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 136.8282° |
| argument of perigee: | 225.0383° |
| revolutions per day: | 14.13713874 |
| mean anomaly at epoch: | 162.9414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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