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 26044.89297911 +.00000000 +00000-0 +79304-4 0 00001
2 11511 74.0331 256.4374 0014421 87.6229 272.6576 14.38264383 03
| Epoch (UTC): | 13 February 2026 21:25:53 |
| Eccentricity: | 0.0014421 |
| inclination: | 74.0331° |
| perigee height: | 754 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 256.4374° |
| argument of perigee: | 87.6229° |
| revolutions per day: | 14.38264383 |
| mean anomaly at epoch: | 272.6576° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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