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 22141.87856742 -.00000037 00000-0 15882-3 0 9992
2 23439 64.8150 188.5961 0167678 277.0424 81.1457 11.27572005128496
| Epoch (UTC): | 21 May 2022 21:05:08 |
| Eccentricity: | 0.0167678 |
| inclination: | 64.8150° |
| perigee height: | 1881 km |
| apogee height: | 2163 km |
| right ascension of ascending node: | 188.5961° |
| argument of perigee: | 277.0424° |
| revolutions per day: | 11.27572005 |
| mean anomaly at epoch: | 81.1457° |
| orbit number at epoch: | 12849 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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