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 26042.14717057 +.00000000 +00000-0 +81097-4 0 00000
2 20046 82.9354 106.7007 0041545 200.5211 159.4280 13.78609976 01
| Epoch (UTC): | 11 February 2026 03:31:55 |
| Eccentricity: | 0.0041545 |
| inclination: | 82.9354° |
| perigee height: | 938 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 106.7007° |
| argument of perigee: | 200.5211° |
| revolutions per day: | 13.78609976 |
| mean anomaly at epoch: | 159.4280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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