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 43232U 26145.35763262 +.00000000 +00000-0 +00000-0 0 00009
2 43232 0.0500 7.9564 0002673 51.6122 300.4573 5.00116001 03
| Epoch (UTC): | 25 May 2026 08:34:59 |
| Eccentricity: | 0.0002673 |
| inclination: | 0.0500° |
| perigee height: | 8062 km |
| apogee height: | 8070 km |
| right ascension of ascending node: | 7.9564° |
| argument of perigee: | 51.6122° |
| revolutions per day: | 5.00116001 |
| mean anomaly at epoch: | 300.4573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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