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 46674U 26145.59059083 +.00000000 +00000-0 +62968-3 0 00001
2 46674 53.0424 211.3507 0002663 306.2504 53.8267 15.69863131 07
| Epoch (UTC): | 25 May 2026 14:10:27 |
| Eccentricity: | 0.0002663 |
| inclination: | 53.0424° |
| perigee height: | 357 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 211.3507° |
| argument of perigee: | 306.2504° |
| revolutions per day: | 15.69863131 |
| mean anomaly at epoch: | 53.8267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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