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 26071.47559707 +.00000000 +00000-0 +73095-4 0 00005
2 12443 74.0514 86.2929 0003071 130.4666 229.6755 14.36033668 06
| Epoch (UTC): | 12 March 2026 11:24:51 |
| Eccentricity: | 0.0003071 |
| inclination: | 74.0514° |
| perigee height: | 769 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 86.2929° |
| argument of perigee: | 130.4666° |
| revolutions per day: | 14.36033668 |
| mean anomaly at epoch: | 229.6755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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