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 39468U 13072G 24358.21909285 .00123610 00000-0 27251-2 0 9993
2 39468 120.4777 178.4656 0092883 171.5309 188.7361 15.38613890 33850
| Epoch (UTC): | 23 December 2024 05:15:29 |
| Eccentricity: | 0.0092883 |
| inclination: | 120.4777° |
| perigee height: | 387 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 178.4656° |
| argument of perigee: | 171.5309° |
| revolutions per day: | 15.38613890 |
| mean anomaly at epoch: | 188.7361° |
| orbit number at epoch: | 3385 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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