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 48593U 26145.37878948 +.00000000 +00000-0 +18030-4 0 00000
2 48593 53.1589 143.2200 0001075 103.3125 256.7996 15.31697489 09
| Epoch (UTC): | 25 May 2026 09:05:27 |
| Eccentricity: | 0.0001075 |
| inclination: | 53.1589° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 143.2200° |
| argument of perigee: | 103.3125° |
| revolutions per day: | 15.31697489 |
| mean anomaly at epoch: | 256.7996° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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