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 47742U 26145.51794704 +.00000000 +00000-0 -73446-4 0 00001
2 47742 53.1584 196.8265 0001738 68.5436 291.5750 15.31707011 05
| Epoch (UTC): | 25 May 2026 12:25:50 |
| Eccentricity: | 0.0001738 |
| inclination: | 53.1584° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 196.8265° |
| argument of perigee: | 68.5436° |
| revolutions per day: | 15.31707011 |
| mean anomaly at epoch: | 291.5750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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