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 46051U 26145.61468737 +.00000000 +00000-0 +12439-3 0 00001
2 46051 53.1596 116.4232 0001233 64.8353 295.2776 15.31713190 03
| Epoch (UTC): | 25 May 2026 14:45:08 |
| Eccentricity: | 0.0001233 |
| inclination: | 53.1596° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 116.4232° |
| argument of perigee: | 64.8353° |
| revolutions per day: | 15.31713190 |
| mean anomaly at epoch: | 295.2776° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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