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 47143U 26145.66668980 +.00000000 +00000-0 +44242-3 0 00008
2 47143 53.0456 259.4933 0003147 2.6182 11.8377 15.67117976 00
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0003147 |
| inclination: | 53.0456° |
| perigee height: | 365 km |
| apogee height: | 369 km |
| right ascension of ascending node: | 259.4933° |
| argument of perigee: | 2.6182° |
| revolutions per day: | 15.67117976 |
| mean anomaly at epoch: | 11.8377° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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