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 20046U 26140.19885431 +.00000000 +00000-0 +61674-4 0 00005
2 20046 82.9386 33.5376 0040593 288.0455 71.6283 13.78632329 01
| Epoch (UTC): | 20 May 2026 04:46:21 |
| Eccentricity: | 0.0040593 |
| inclination: | 82.9386° |
| perigee height: | 939 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 33.5376° |
| argument of perigee: | 288.0455° |
| revolutions per day: | 13.78632329 |
| mean anomaly at epoch: | 71.6283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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