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 40012U 26073.38168125 +.00000000 +00000-0 +42208-3 0 00001
2 40012 97.7730 227.8671 0045760 22.5980 337.7238 14.87674800 01
| Epoch (UTC): | 14 March 2026 09:09:37 |
| Eccentricity: | 0.0045760 |
| inclination: | 97.7730° |
| perigee height: | 573 km |
| apogee height: | 637 km |
| right ascension of ascending node: | 227.8671° |
| argument of perigee: | 22.5980° |
| revolutions per day: | 14.87674800 |
| mean anomaly at epoch: | 337.7238° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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