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 23463U 95002A 23343.09114236 .00000070 00000-0 59052-4 0 9997
2 23463 82.9263 337.0486 0038993 175.9161 249.4098 13.72598203446362
| Epoch (UTC): | 09 December 2023 02:11:14 |
| Eccentricity: | 0.0038993 |
| inclination: | 82.9263° |
| perigee height: | 961 km |
| apogee height: | 1019 km |
| right ascension of ascending node: | 337.0486° |
| argument of perigee: | 175.9161° |
| revolutions per day: | 13.72598203 |
| mean anomaly at epoch: | 249.4098° |
| orbit number at epoch: | 44636 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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