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 11511U 26037.65911766 +.00000000 +00000-0 +91885-4 0 00006
2 11511 74.0343 269.7674 0014338 103.8134 256.4616 14.38260994 08
| Epoch (UTC): | 06 February 2026 15:49:07 |
| Eccentricity: | 0.0014338 |
| inclination: | 74.0343° |
| perigee height: | 754 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 269.7674° |
| argument of perigee: | 103.8134° |
| revolutions per day: | 14.38260994 |
| mean anomaly at epoch: | 256.4616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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