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 23337.16986998 .00003301 00000-0 49533-3 0 9995
2 39161 97.8545 44.5698 0010028 140.3833 219.8111 14.75196334568071
| Epoch (UTC): | 03 December 2023 04:04:36 |
| Eccentricity: | 0.0010028 |
| inclination: | 97.8545° |
| perigee height: | 637 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 44.5698° |
| argument of perigee: | 140.3833° |
| revolutions per day: | 14.75196334 |
| mean anomaly at epoch: | 219.8111° |
| orbit number at epoch: | 56807 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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