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 48009U 26145.43896194 +.00000000 +00000-0 +32577-4 0 00004
2 48009 53.1591 312.4422 0001664 85.1022 275.0170 15.31696641 04
| Epoch (UTC): | 25 May 2026 10:32:06 |
| Eccentricity: | 0.0001664 |
| inclination: | 53.1591° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 312.4422° |
| argument of perigee: | 85.1022° |
| revolutions per day: | 15.31696641 |
| mean anomaly at epoch: | 275.0170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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