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 47843U 26144.81043249 +.00000000 +00000-0 +17327-3 0 00000
2 47843 53.1577 261.2531 0001171 86.7265 273.3870 15.31726611 03
| Epoch (UTC): | 24 May 2026 19:27:01 |
| Eccentricity: | 0.0001171 |
| inclination: | 53.1577° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 261.2531° |
| argument of perigee: | 86.7265° |
| revolutions per day: | 15.31726611 |
| mean anomaly at epoch: | 273.3870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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