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 23030.90483271 .00002355 00000-0 95976-3 0 9999
2 00020 33.3554 9.5521 1660564 308.0593 38.1229 11.56648644341429
| Epoch (UTC): | 30 January 2023 21:42:57 |
| Eccentricity: | 0.1660564 |
| inclination: | 33.3554° |
| perigee height: | 509 km |
| apogee height: | 3252 km |
| right ascension of ascending node: | 9.5521° |
| argument of perigee: | 308.0593° |
| revolutions per day: | 11.56648644 |
| mean anomaly at epoch: | 38.1229° |
| orbit number at epoch: | 34142 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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