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 48563U 26145.23985149 +.00000000 +00000-0 +29806-4 0 00007
2 48563 53.1583 130.6865 0001289 80.1143 280.0004 15.31704036 03
| Epoch (UTC): | 25 May 2026 05:45:23 |
| Eccentricity: | 0.0001289 |
| inclination: | 53.1583° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 130.6865° |
| argument of perigee: | 80.1143° |
| revolutions per day: | 15.31704036 |
| mean anomaly at epoch: | 280.0004° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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