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 00046U 26046.84539519 +.00000000 +00000-0 +12988-3 0 00006
2 00046 66.6873 199.0101 0192656 22.5072 338.4346 14.54650483 07
| Epoch (UTC): | 15 February 2026 20:17:22 |
| Eccentricity: | 0.0192656 |
| inclination: | 66.6873° |
| perigee height: | 574 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 199.0101° |
| argument of perigee: | 22.5072° |
| revolutions per day: | 14.54650483 |
| mean anomaly at epoch: | 338.4346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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