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 48570U 26145.66668980 +.00000000 +00000-0 +17801-1 0 00002
2 48570 53.1255 149.5691 0001630 90.2424 231.3972 15.53913972 05
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001630 |
| inclination: | 53.1255° |
| perigee height: | 404 km |
| apogee height: | 406 km |
| right ascension of ascending node: | 149.5691° |
| argument of perigee: | 90.2424° |
| revolutions per day: | 15.53913972 |
| mean anomaly at epoch: | 231.3972° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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