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 23030.24006168 .00001304 00000-0 78868-3 0 9991
2 12 32.8947 242.3255 1661102 67.8430 308.9761 11.44927335632202
| Epoch (UTC): | 30 January 2023 05:45:41 |
| Eccentricity: | 0.1661102 |
| inclination: | 32.8947° |
| perigee height: | 556 km |
| apogee height: | 3318 km |
| right ascension of ascending node: | 242.3255° |
| argument of perigee: | 67.8430° |
| revolutions per day: | 11.44927335 |
| mean anomaly at epoch: | 308.9761° |
| orbit number at epoch: | 63220 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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