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 23159.38363934 .00000580 00000-0 70039-4 0 9993
2 20466 82.5014 130.2988 0020760 14.1456 346.0335 14.81905966779519
| Epoch (UTC): | 08 June 2023 09:12:26 |
| Eccentricity: | 0.0020760 |
| inclination: | 82.5014° |
| perigee height: | 609 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 130.2988° |
| argument of perigee: | 14.1456° |
| revolutions per day: | 14.81905966 |
| mean anomaly at epoch: | 346.0335° |
| orbit number at epoch: | 77951 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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