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 00020U 59007A 23270.27214153 .00001181 00000-0 47954-3 0 9995
2 00020 33.3405 234.2673 1656326 141.6364 231.4506 11.57838988369167
| Epoch (UTC): | 27 September 2023 06:31:53 |
| Eccentricity: | 0.1656326 |
| inclination: | 33.3405° |
| perigee height: | 508 km |
| apogee height: | 3242 km |
| right ascension of ascending node: | 234.2673° |
| argument of perigee: | 141.6364° |
| revolutions per day: | 11.57838988 |
| mean anomaly at epoch: | 231.4506° |
| orbit number at epoch: | 36916 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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