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 23030.85078601 .00001225 00000-0 74078-3 0 9990
2 00012 32.8946 240.1865 1661107 71.0574 306.2250 11.44928802389680
| Epoch (UTC): | 30 January 2023 20:25:07 |
| Eccentricity: | 0.1661107 |
| inclination: | 32.8946° |
| perigee height: | 556 km |
| apogee height: | 3318 km |
| right ascension of ascending node: | 240.1865° |
| argument of perigee: | 71.0574° |
| revolutions per day: | 11.44928802 |
| mean anomaly at epoch: | 306.2250° |
| orbit number at epoch: | 38968 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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