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 23711U 26067.06898895 +.00000000 +00000-0 +95917-4 0 00006
2 23711 100.5075 97.1034 0367197 325.0656 55.1962 13.12851709 03
| Epoch (UTC): | 08 March 2026 01:39:20 |
| Eccentricity: | 0.0367197 |
| inclination: | 100.5075° |
| perigee height: | 933 km |
| apogee height: | 1491 km |
| right ascension of ascending node: | 97.1034° |
| argument of perigee: | 325.0656° |
| revolutions per day: | 13.12851709 |
| mean anomaly at epoch: | 55.1962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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