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 23089.86590642 -.00000039 00000-0 10000-3 0 9996
2 23439 64.8150 42.3652 0165014 223.8713 134.9006 11.27574036163786
| Epoch (UTC): | 30 March 2023 20:46:54 |
| Eccentricity: | 0.0165014 |
| inclination: | 64.8150° |
| perigee height: | 1884 km |
| apogee height: | 2161 km |
| right ascension of ascending node: | 42.3652° |
| argument of perigee: | 223.8713° |
| revolutions per day: | 11.27574036 |
| mean anomaly at epoch: | 134.9006° |
| orbit number at epoch: | 16378 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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