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 15751U 26053.66962647 +.00000000 +00000-0 +68972-4 0 00000
2 15751 82.9526 150.9648 0027661 56.8376 57.7630 13.71926970 06
| Epoch (UTC): | 22 February 2026 16:04:15 |
| Eccentricity: | 0.0027661 |
| inclination: | 82.9526° |
| perigee height: | 972 km |
| apogee height: | 1013 km |
| right ascension of ascending node: | 150.9648° |
| argument of perigee: | 56.8376° |
| revolutions per day: | 13.71926970 |
| mean anomaly at epoch: | 57.7630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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