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 43234U 26139.06780044 +.00000000 +00000-0 +00000-0 0 00009
2 43234 0.0490 326.2733 0003182 43.4287 350.3051 5.00115546 03
| Epoch (UTC): | 19 May 2026 01:37:37 |
| Eccentricity: | 0.0003182 |
| inclination: | 0.0490° |
| perigee height: | 8061 km |
| apogee height: | 8070 km |
| right ascension of ascending node: | 326.2733° |
| argument of perigee: | 43.4287° |
| revolutions per day: | 5.00115546 |
| mean anomaly at epoch: | 350.3051° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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