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 39161U 13021C 24358.17349463 .00004458 00000-0 61822-3 0 9999
2 39161 97.8064 58.8947 0008218 345.9846 14.1136 14.78411397625032
| Epoch (UTC): | 23 December 2024 04:09:49 |
| Eccentricity: | 0.0008218 |
| inclination: | 97.8064° |
| perigee height: | 628 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 58.8947° |
| argument of perigee: | 345.9846° |
| revolutions per day: | 14.78411397 |
| mean anomaly at epoch: | 14.1136° |
| orbit number at epoch: | 62503 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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