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 46080U 26145.04668341 +.00000000 +00000-0 +66044-3 0 00004
2 46080 53.0604 26.8370 0004284 54.9591 305.1820 15.52745526 06
| Epoch (UTC): | 25 May 2026 01:07:13 |
| Eccentricity: | 0.0004284 |
| inclination: | 53.0604° |
| perigee height: | 406 km |
| apogee height: | 412 km |
| right ascension of ascending node: | 26.8370° |
| argument of perigee: | 54.9591° |
| revolutions per day: | 15.52745526 |
| mean anomaly at epoch: | 305.1820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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