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 00012U 59001B 23036.87005442 .00001666 00000-0 10018-2 0 9993
2 00012 32.8936 219.1048 1661063 102.7399 276.3241 11.44948333390372
| Epoch (UTC): | 05 February 2023 20:52:52 |
| Eccentricity: | 0.1661063 |
| inclination: | 32.8936° |
| perigee height: | 556 km |
| apogee height: | 3318 km |
| right ascension of ascending node: | 219.1048° |
| argument of perigee: | 102.7399° |
| revolutions per day: | 11.44948333 |
| mean anomaly at epoch: | 276.3241° |
| orbit number at epoch: | 39037 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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