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 46128U 26145.45152891 +.00000000 +00000-0 +74643-3 0 00004
2 46128 53.0167 203.4852 0007016 15.6551 344.4685 15.79672615 09
| Epoch (UTC): | 25 May 2026 10:50:12 |
| Eccentricity: | 0.0007016 |
| inclination: | 53.0167° |
| perigee height: | 327 km |
| apogee height: | 336 km |
| right ascension of ascending node: | 203.4852° |
| argument of perigee: | 15.6551° |
| revolutions per day: | 15.79672615 |
| mean anomaly at epoch: | 344.4685° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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