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 23089.19598542 .00004098 00000-0 24427-2 0 9995
2 12 32.9011 35.7896 1660108 18.2631 347.0988 11.45310102638950
| Epoch (UTC): | 30 March 2023 04:42:13 |
| Eccentricity: | 0.1660108 |
| inclination: | 32.9011° |
| perigee height: | 555 km |
| apogee height: | 3315 km |
| right ascension of ascending node: | 35.7896° |
| argument of perigee: | 18.2631° |
| revolutions per day: | 11.45310102 |
| mean anomaly at epoch: | 347.0988° |
| orbit number at epoch: | 63895 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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