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 48107U 26145.29330992 +.00000000 +00000-0 -60556-4 0 00005
2 48107 53.1607 156.4986 0001303 86.1907 273.9243 15.31688852 08
| Epoch (UTC): | 25 May 2026 07:02:21 |
| Eccentricity: | 0.0001303 |
| inclination: | 53.1607° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 156.4986° |
| argument of perigee: | 86.1907° |
| revolutions per day: | 15.31688852 |
| mean anomaly at epoch: | 273.9243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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