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 20642U 90050E 24128.84789741 0.00007500 00000-0 60349-3 0 03
2 20642 63.2937 114.7819 0916293 68.0025 291.9975 13.51384413 03
| Epoch (UTC): | 07 May 2024 20:20:58 |
| Eccentricity: | 0.0916293 |
| inclination: | 63.2937° |
| perigee height: | 385 km |
| apogee height: | 1749 km |
| right ascension of ascending node: | 114.7819° |
| argument of perigee: | 68.0025° |
| revolutions per day: | 13.51384413 |
| mean anomaly at epoch: | 291.9975° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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