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 39471U 13072K 24358.10691223 .00020031 00000-0 11964-2 0 9992
2 39471 120.4731 61.6628 0209148 145.3049 216.1850 14.94721676 33942
| Epoch (UTC): | 23 December 2024 02:33:57 |
| Eccentricity: | 0.0209148 |
| inclination: | 120.4731° |
| perigee height: | 437 km |
| apogee height: | 729 km |
| right ascension of ascending node: | 61.6628° |
| argument of perigee: | 145.3049° |
| revolutions per day: | 14.94721676 |
| mean anomaly at epoch: | 216.1850° |
| orbit number at epoch: | 3394 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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