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 43772U 26100.18384875 +.00000000 +00000-0 +13247-2 0 00008
2 43772 97.4223 177.0668 0000914 200.9511 159.1710 15.64897001 04
| Epoch (UTC): | 10 April 2026 04:24:44 |
| Eccentricity: | 0.0000914 |
| inclination: | 97.4223° |
| perigee height: | 373 km |
| apogee height: | 374 km |
| right ascension of ascending node: | 177.0668° |
| argument of perigee: | 200.9511° |
| revolutions per day: | 15.64897001 |
| mean anomaly at epoch: | 159.1710° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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