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 29658U 06060A 20331.21443851 0.00001600 00000-0 59298-4 0 06
2 29658 98.1628 152.4278 0003262 329.7205 30.2794 15.27656907 09
| Epoch (UTC): | 26 November 2020 05:08:47 |
| Eccentricity: | 0.0003262 |
| inclination: | 98.1628° |
| perigee height: | 480 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 152.4278° |
| argument of perigee: | 329.7205° |
| revolutions per day: | 15.27656907 |
| mean anomaly at epoch: | 30.2794° |
| 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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