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 43276U 26145.61837492 +.00000000 +00000-0 -17373-3 0 00008
2 43276 63.3930 149.3578 0273435 7.2818 353.2056 13.45454228 07
| Epoch (UTC): | 25 May 2026 14:50:27 |
| Eccentricity: | 0.0273435 |
| inclination: | 63.3930° |
| perigee height: | 885 km |
| apogee height: | 1293 km |
| right ascension of ascending node: | 149.3578° |
| argument of perigee: | 7.2818° |
| revolutions per day: | 13.45454228 |
| mean anomaly at epoch: | 353.2056° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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