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 46047U 26145.63329946 +.00000000 +00000-0 -26705-5 0 00000
2 46047 53.1607 116.1513 0001178 102.6389 257.4744 15.31700261 08
| Epoch (UTC): | 25 May 2026 15:11:57 |
| Eccentricity: | 0.0001178 |
| inclination: | 53.1607° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 116.1513° |
| argument of perigee: | 102.6389° |
| revolutions per day: | 15.31700261 |
| mean anomaly at epoch: | 257.4744° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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