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 46053U 26145.19519178 +.00000000 +00000-0 +19749-4 0 00004
2 46053 53.1589 118.1872 0001234 85.3237 274.7906 15.31701224 08
| Epoch (UTC): | 25 May 2026 04:41:04 |
| Eccentricity: | 0.0001234 |
| inclination: | 53.1589° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 118.1872° |
| argument of perigee: | 85.3237° |
| revolutions per day: | 15.31701224 |
| mean anomaly at epoch: | 274.7906° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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