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 48042U 26145.47478867 +.00000000 +00000-0 +58872-3 0 00003
2 48042 87.8947 324.7475 0001803 89.5578 270.5757 13.13468839 08
| Epoch (UTC): | 25 May 2026 11:23:41 |
| Eccentricity: | 0.0001803 |
| inclination: | 87.8947° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7475° |
| argument of perigee: | 89.5578° |
| revolutions per day: | 13.13468839 |
| mean anomaly at epoch: | 270.5757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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