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 46083U 26145.61159795 +.00000000 +00000-0 +85366-4 0 00007
2 46083 53.1617 103.4229 0001432 102.9997 257.1164 15.31697775 01
| Epoch (UTC): | 25 May 2026 14:40:42 |
| Eccentricity: | 0.0001432 |
| inclination: | 53.1617° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 103.4229° |
| argument of perigee: | 102.9997° |
| revolutions per day: | 15.31697775 |
| mean anomaly at epoch: | 257.1164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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