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 46070U 26145.31305154 +.00000000 +00000-0 +37985-4 0 00006
2 46070 53.1591 105.3880 0000956 87.5735 272.5375 15.31702426 05
| Epoch (UTC): | 25 May 2026 07:30:47 |
| Eccentricity: | 0.0000956 |
| inclination: | 53.1591° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 105.3880° |
| argument of perigee: | 87.5735° |
| revolutions per day: | 15.31702426 |
| mean anomaly at epoch: | 272.5375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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