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 23439U 94085A 23033.54771307 -.00000039 00000-0 10000-3 0 9999
2 23439 64.8177 133.4527 0166288 233.3746 125.1785 11.27573343157435
| Epoch (UTC): | 02 February 2023 13:08:42 |
| Eccentricity: | 0.0166288 |
| inclination: | 64.8177° |
| perigee height: | 1882 km |
| apogee height: | 2162 km |
| right ascension of ascending node: | 133.4527° |
| argument of perigee: | 233.3746° |
| revolutions per day: | 11.27573343 |
| mean anomaly at epoch: | 125.1785° |
| orbit number at epoch: | 15743 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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