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 20466U 26042.11275670 +.00000000 +00000-0 +54579-4 0 00008
2 20466 82.5024 292.3547 0020652 31.3571 328.8871 14.83545760 08
| Epoch (UTC): | 11 February 2026 02:42:22 |
| Eccentricity: | 0.0020652 |
| inclination: | 82.5024° |
| perigee height: | 604 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 292.3547° |
| argument of perigee: | 31.3571° |
| revolutions per day: | 14.83545760 |
| mean anomaly at epoch: | 328.8871° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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