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 43476U 18047A 22270.59870363 +.00002537 00000-0 +10210-3 0 05
2 43476 88.9947 24.6452 0012924 330.7988 129.9301 15.24769213241989
| Epoch (UTC): | 27 September 2022 14:22:07 |
| Eccentricity: | 0.0012924 |
| inclination: | 88.9947° |
| perigee height: | 482 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 24.6452° |
| argument of perigee: | 330.7988° |
| revolutions per day: | 15.24769213 |
| mean anomaly at epoch: | 129.9301° |
| orbit number at epoch: | 24198 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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