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 26137.51664420 +.00000000 +00000-0 +54817-4 0 00003
2 12443 74.0535 325.1770 0004506 330.0320 30.0574 14.36063205 00
| Epoch (UTC): | 17 May 2026 12:23:58 |
| Eccentricity: | 0.0004506 |
| inclination: | 74.0535° |
| perigee height: | 768 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 325.1770° |
| argument of perigee: | 330.0320° |
| revolutions per day: | 14.36063205 |
| mean anomaly at epoch: | 30.0574° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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