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 23341.47940617 -.00000054 00000-0 -31478-3 0 9995
2 23439 64.8187 355.4197 0156675 179.5236 180.5862 11.27575470191868
| Epoch (UTC): | 07 December 2023 11:30:20 |
| Eccentricity: | 0.0156675 |
| inclination: | 64.8187° |
| perigee height: | 1891 km |
| apogee height: | 2154 km |
| right ascension of ascending node: | 355.4197° |
| argument of perigee: | 179.5236° |
| revolutions per day: | 11.27575470 |
| mean anomaly at epoch: | 180.5862° |
| orbit number at epoch: | 19186 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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