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 23318U 94066B 24257.42917753 .00002009 00000-0 26131-3 0 9997
2 23318 82.5390 234.5375 0022335 209.6906 150.3041 14.80043567613633
| Epoch (UTC): | 13 September 2024 10:18:00 |
| Eccentricity: | 0.0022335 |
| inclination: | 82.5390° |
| perigee height: | 613 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 234.5375° |
| argument of perigee: | 209.6906° |
| revolutions per day: | 14.80043567 |
| mean anomaly at epoch: | 150.3041° |
| orbit number at epoch: | 61363 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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