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 23026.92451180 .00001975 00000-0 11900-2 0 9996
2 12 32.8945 253.9383 1661144 50.3933 323.1936 11.44917743631823
| Epoch (UTC): | 26 January 2023 22:11:17 |
| Eccentricity: | 0.1661144 |
| inclination: | 32.8945° |
| perigee height: | 556 km |
| apogee height: | 3318 km |
| right ascension of ascending node: | 253.9383° |
| argument of perigee: | 50.3933° |
| revolutions per day: | 11.44917743 |
| mean anomaly at epoch: | 323.1936° |
| orbit number at epoch: | 63182 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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