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 46075U 26145.61471775 +.00000000 +00000-0 -13006-4 0 00006
2 46075 53.1615 103.7566 0001310 77.3634 282.7514 15.30183404 06
| Epoch (UTC): | 25 May 2026 14:45:11 |
| Eccentricity: | 0.0001310 |
| inclination: | 53.1615° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 103.7566° |
| argument of perigee: | 77.3634° |
| revolutions per day: | 15.30183404 |
| mean anomaly at epoch: | 282.7514° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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