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 43231U 26145.50518183 +.00000000 +00000-0 +00000-0 0 00005
2 43231 0.0512 3.4697 0002634 57.0566 299.4996 5.00115791 03
| Epoch (UTC): | 25 May 2026 12:07:27 |
| Eccentricity: | 0.0002634 |
| inclination: | 0.0512° |
| perigee height: | 8062 km |
| apogee height: | 8070 km |
| right ascension of ascending node: | 3.4697° |
| argument of perigee: | 57.0566° |
| revolutions per day: | 5.00115791 |
| mean anomaly at epoch: | 299.4996° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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