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 26139.95484448 +.00000000 +00000-0 +37613-4 0 00008
2 12443 74.0534 320.7048 0004650 325.5943 34.4908 14.36063317 01
| Epoch (UTC): | 19 May 2026 22:54:58 |
| Eccentricity: | 0.0004650 |
| inclination: | 74.0534° |
| perigee height: | 768 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 320.7048° |
| argument of perigee: | 325.5943° |
| revolutions per day: | 14.36063317 |
| mean anomaly at epoch: | 34.4908° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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