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 27168U 02001A 23270.76312999 .00000091 00000-0 00000+0 0 9996
2 27168 10.0141 27.0407 0098223 355.3053 277.5763 1.00270351 21684
| Epoch (UTC): | 27 September 2023 18:18:54 |
| Eccentricity: | 0.0098223 |
| inclination: | 10.0141° |
| perigee height: | 35372 km |
| apogee height: | 36201 km |
| right ascension of ascending node: | 27.0407° |
| argument of perigee: | 355.3053° |
| revolutions per day: | 1.00270351 |
| mean anomaly at epoch: | 277.5763° |
| orbit number at epoch: | 2168 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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