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 15769U 26100.15133492 +.00000000 +00000-0 +19776-4 0 00002
2 15769 81.2732 256.6666 0062902 117.1004 243.6601 14.07243089 03
| Epoch (UTC): | 10 April 2026 03:37:55 |
| Eccentricity: | 0.0062902 |
| inclination: | 81.2732° |
| perigee height: | 823 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 256.6666° |
| argument of perigee: | 117.1004° |
| revolutions per day: | 14.07243089 |
| mean anomaly at epoch: | 243.6601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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