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 48139U 26145.45142566 +.00000000 +00000-0 +62554-4 0 00005
2 48139 53.1578 155.7095 0001232 83.0281 277.0860 15.31709341 02
| Epoch (UTC): | 25 May 2026 10:50:03 |
| Eccentricity: | 0.0001232 |
| inclination: | 53.1578° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 155.7095° |
| argument of perigee: | 83.0281° |
| revolutions per day: | 15.31709341 |
| mean anomaly at epoch: | 277.0860° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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