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 24091U 26110.36656685 +.00000000 +00000-0 +23273-3 0 00004
2 24091 81.9922 76.1714 0062544 24.5452 127.5910 15.06495298 02
| Epoch (UTC): | 20 April 2026 08:47:51 |
| Eccentricity: | 0.0062544 |
| inclination: | 81.9922° |
| perigee height: | 504 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 76.1714° |
| argument of perigee: | 24.5452° |
| revolutions per day: | 15.06495298 |
| mean anomaly at epoch: | 127.5910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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