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 data is extracted from the following two-line orbital elements,
1 20466U 90010B 23152.42884292 .00000520 00000-0 62499-4 0 9991
2 20466 82.5011 136.8133 0021332 36.2192 324.0461 14.81898514778489
| Epoch (UTC): | 01 June 2023 10:17:32 |
| Eccentricity: | 0.0021332 |
| inclination: | 82.5011° |
| perigee height: | 608 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 136.8133° |
| argument of perigee: | 36.2192° |
| revolutions per day: | 14.81898514 |
| mean anomaly at epoch: | 324.0461° |
| orbit number at epoch: | 77848 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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