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 39168U 13024A 23081.75154067 -.00000299 00000-0 00000+0 0 9996
2 39168 0.0096 160.4288 0000175 225.1732 12.4076 1.00270386 35979
| Epoch (UTC): | 22 March 2023 18:02:13 |
| Eccentricity: | 0.0000175 |
| inclination: | 0.0096° |
| perigee height: | 35786 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 160.4288° |
| argument of perigee: | 225.1732° |
| revolutions per day: | 1.00270386 |
| mean anomaly at epoch: | 12.4076° |
| orbit number at epoch: | 3597 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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