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 26044.71400172 +.00000000 +00000-0 +12459-3 0 00005
2 00046 66.6870 204.8184 0192477 24.1323 336.8656 14.54647032 00
| Epoch (UTC): | 13 February 2026 17:08:09 |
| Eccentricity: | 0.0192477 |
| inclination: | 66.6870° |
| perigee height: | 574 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 204.8184° |
| argument of perigee: | 24.1323° |
| revolutions per day: | 14.54647032 |
| mean anomaly at epoch: | 336.8656° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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