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 12U 59001B 23032.59564378 .00001335 00000-0 80633-3 0 9990
2 12 32.8943 234.0757 1661112 80.2397 298.1032 11.44933950632475
| Epoch (UTC): | 01 February 2023 14:17:43 |
| Eccentricity: | 0.1661112 |
| inclination: | 32.8943° |
| perigee height: | 556 km |
| apogee height: | 3318 km |
| right ascension of ascending node: | 234.0757° |
| argument of perigee: | 80.2397° |
| revolutions per day: | 11.44933950 |
| mean anomaly at epoch: | 298.1032° |
| orbit number at epoch: | 63247 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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