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 23085.96354362 -.00000039 00000-0 10000-3 0 9990
2 23439 64.8145 48.6758 0165027 224.5764 134.1788 11.27574059163340
| Epoch (UTC): | 26 March 2023 23:07:30 |
| Eccentricity: | 0.0165027 |
| inclination: | 64.8145° |
| perigee height: | 1884 km |
| apogee height: | 2161 km |
| right ascension of ascending node: | 48.6758° |
| argument of perigee: | 224.5764° |
| revolutions per day: | 11.27574059 |
| mean anomaly at epoch: | 134.1788° |
| orbit number at epoch: | 16334 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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