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 00012U 26131.89540868 +.00000000 +00000-0 +47539-4 0 00009
2 00012 32.9145 353.1149 1647180 273.0026 68.4099 11.48608181 06
| Epoch (UTC): | 11 May 2026 21:29:23 |
| Eccentricity: | 0.1647180 |
| inclination: | 32.9145° |
| perigee height: | 553 km |
| apogee height: | 3286 km |
| right ascension of ascending node: | 353.1149° |
| argument of perigee: | 273.0026° |
| revolutions per day: | 11.48608181 |
| mean anomaly at epoch: | 68.4099° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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