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 23335.74546148 .00004230 00000-0 63281-3 0 9994
2 39161 97.8546 43.1874 0009939 144.5789 215.6083 14.75184912567865
| Epoch (UTC): | 01 December 2023 17:53:27 |
| Eccentricity: | 0.0009939 |
| inclination: | 97.8546° |
| perigee height: | 637 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 43.1874° |
| argument of perigee: | 144.5789° |
| revolutions per day: | 14.75184912 |
| mean anomaly at epoch: | 215.6083° |
| orbit number at epoch: | 56786 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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