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 48106U 26145.46074406 +.00000000 +00000-0 +17866-4 0 00003
2 48106 53.1603 155.5929 0001136 83.2219 276.8912 15.31702614 06
| Epoch (UTC): | 25 May 2026 11:03:28 |
| Eccentricity: | 0.0001136 |
| inclination: | 53.1603° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 155.5929° |
| argument of perigee: | 83.2219° |
| revolutions per day: | 15.31702614 |
| mean anomaly at epoch: | 276.8912° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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