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 06393U 26037.64087196 +.00000000 +00000-0 -32904-4 0 00006
2 06393 81.2583 145.1089 0059249 49.5475 311.0838 14.05422878 06
| Epoch (UTC): | 06 February 2026 15:22:51 |
| Eccentricity: | 0.0059249 |
| inclination: | 81.2583° |
| perigee height: | 832 km |
| apogee height: | 918 km |
| right ascension of ascending node: | 145.1089° |
| argument of perigee: | 49.5475° |
| revolutions per day: | 14.05422878 |
| mean anomaly at epoch: | 311.0838° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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