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 26088.17886766 +.00000000 +00000-0 +76173-4 0 00002
2 20466 82.4998 249.0765 0018612 233.1178 126.8332 14.83587281 08
| Epoch (UTC): | 29 March 2026 04:17:34 |
| Eccentricity: | 0.0018612 |
| inclination: | 82.4998° |
| perigee height: | 605 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 249.0765° |
| argument of perigee: | 233.1178° |
| revolutions per day: | 14.83587281 |
| mean anomaly at epoch: | 126.8332° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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