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 47834U 26144.77508744 +.00000000 +00000-0 +29806-3 0 00006
2 47834 53.1586 251.1774 0001087 74.4306 285.6815 15.31733367 07
| Epoch (UTC): | 24 May 2026 18:36:07 |
| Eccentricity: | 0.0001087 |
| inclination: | 53.1586° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 251.1774° |
| argument of perigee: | 74.4306° |
| revolutions per day: | 15.31733367 |
| mean anomaly at epoch: | 285.6815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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