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 43706U 26144.20755413 +.00000000 +00000-0 +00000-0 0 00007
2 43706 54.1673 183.1096 0009838 291.2944 109.0036 1.86228425 02
| Epoch (UTC): | 24 May 2026 04:58:52 |
| Eccentricity: | 0.0009838 |
| inclination: | 54.1673° |
| perigee height: | 21501 km |
| apogee height: | 21556 km |
| right ascension of ascending node: | 183.1096° |
| argument of perigee: | 291.2944° |
| revolutions per day: | 1.86228425 |
| mean anomaly at epoch: | 109.0036° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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