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 23161.16175534 .00001825 00000-0 28305-3 0 9999
2 39161 97.8718 233.6258 0009049 2.2441 357.8806 14.74299713542135
| Epoch (UTC): | 10 June 2023 03:52:55 |
| Eccentricity: | 0.0009049 |
| inclination: | 97.8718° |
| perigee height: | 641 km |
| apogee height: | 654 km |
| right ascension of ascending node: | 233.6258° |
| argument of perigee: | 2.2441° |
| revolutions per day: | 14.74299713 |
| mean anomaly at epoch: | 357.8806° |
| orbit number at epoch: | 54213 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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