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 24340.55097228 -.00000048 00000-0 -17134-3 0 9991
2 23439 64.8140 126.6438 0146418 110.8368 250.8305 11.27580417232913
| Epoch (UTC): | 05 December 2024 13:13:24 |
| Eccentricity: | 0.0146418 |
| inclination: | 64.8140° |
| perigee height: | 1899 km |
| apogee height: | 2145 km |
| right ascension of ascending node: | 126.6438° |
| argument of perigee: | 110.8368° |
| revolutions per day: | 11.27580417 |
| mean anomaly at epoch: | 250.8305° |
| orbit number at epoch: | 23291 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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