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 48126U 26145.40478352 +.00000000 +00000-0 +28913-4 0 00002
2 48126 53.1583 155.6577 0001534 94.0504 266.0673 15.31691325 05
| Epoch (UTC): | 25 May 2026 09:42:53 |
| Eccentricity: | 0.0001534 |
| inclination: | 53.1583° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 155.6577° |
| argument of perigee: | 94.0504° |
| revolutions per day: | 15.31691325 |
| mean anomaly at epoch: | 266.0673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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