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 48385U 26144.99105762 +.00000000 +00000-0 +55702-4 0 00000
2 48385 53.1603 350.5397 0001201 85.1675 274.9464 15.31697117 03
| Epoch (UTC): | 24 May 2026 23:47:07 |
| Eccentricity: | 0.0001201 |
| inclination: | 53.1603° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 350.5397° |
| argument of perigee: | 85.1675° |
| revolutions per day: | 15.31697117 |
| mean anomaly at epoch: | 274.9464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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