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 12443U 26088.19499078 +.00000000 +00000-0 +92513-4 0 00002
2 12443 74.0534 55.6272 0002923 82.5904 277.5580 14.36040759 03
| Epoch (UTC): | 29 March 2026 04:40:47 |
| Eccentricity: | 0.0002923 |
| inclination: | 74.0534° |
| perigee height: | 770 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 55.6272° |
| argument of perigee: | 82.5904° |
| revolutions per day: | 14.36040759 |
| mean anomaly at epoch: | 277.5580° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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