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 47354U 26145.65743289 +.00000000 +00000-0 +47695-4 0 00003
2 47354 53.1618 25.9971 0001439 90.2442 269.8724 15.31698716 05
| Epoch (UTC): | 25 May 2026 15:46:42 |
| Eccentricity: | 0.0001439 |
| inclination: | 53.1618° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 25.9971° |
| argument of perigee: | 90.2442° |
| revolutions per day: | 15.31698716 |
| mean anomaly at epoch: | 269.8724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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