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 23083.92367190 -.00000039 00000-0 10000-3 0 9997
2 23439 64.8144 51.9744 0165040 224.9307 133.8158 11.27574103163115
| Epoch (UTC): | 24 March 2023 22:10:05 |
| Eccentricity: | 0.0165040 |
| inclination: | 64.8144° |
| perigee height: | 1884 km |
| apogee height: | 2161 km |
| right ascension of ascending node: | 51.9744° |
| argument of perigee: | 224.9307° |
| revolutions per day: | 11.27574103 |
| mean anomaly at epoch: | 133.8158° |
| orbit number at epoch: | 16311 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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