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 25346.33676213 -.00000025 00000-0 50582-3 0 9999
2 23439 64.8158 245.4024 0149667 38.5818 322.5690 11.27582941274833
| Epoch (UTC): | 12 December 2025 08:04:56 |
| Eccentricity: | 0.0149667 |
| inclination: | 64.8158° |
| perigee height: | 1896 km |
| apogee height: | 2148 km |
| right ascension of ascending node: | 245.4024° |
| argument of perigee: | 38.5818° |
| revolutions per day: | 11.27582941 |
| mean anomaly at epoch: | 322.5690° |
| orbit number at epoch: | 27483 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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