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 47793U 26144.99271312 +.00000000 +00000-0 +41974-3 0 00002
2 47793 53.1614 244.2517 0000889 84.3178 275.7925 15.31703258 05
| Epoch (UTC): | 24 May 2026 23:49:30 |
| Eccentricity: | 0.0000889 |
| inclination: | 53.1614° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 244.2517° |
| argument of perigee: | 84.3178° |
| revolutions per day: | 15.31703258 |
| mean anomaly at epoch: | 275.7925° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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