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 20437U 90005B 23271.94611542 .00000242 00000-0 10637-3 0 9995
2 20437 98.9080 282.1772 0009522 293.0393 128.7230 14.32644944759485
| Epoch (UTC): | 28 September 2023 22:42:24 |
| Eccentricity: | 0.0009522 |
| inclination: | 98.9080° |
| perigee height: | 776 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 282.1772° |
| argument of perigee: | 293.0393° |
| revolutions per day: | 14.32644944 |
| mean anomaly at epoch: | 128.7230° |
| orbit number at epoch: | 75948 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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