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 24279.88732096 -.00000027 00000-0 43097-3 0 9990
2 23439 64.8157 224.7444 0147208 122.7187 238.8026 11.27578863226075
| Epoch (UTC): | 05 October 2024 21:17:44 |
| Eccentricity: | 0.0147208 |
| inclination: | 64.8157° |
| perigee height: | 1898 km |
| apogee height: | 2146 km |
| right ascension of ascending node: | 224.7444° |
| argument of perigee: | 122.7187° |
| revolutions per day: | 11.27578863 |
| mean anomaly at epoch: | 238.8026° |
| orbit number at epoch: | 22607 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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