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 32958U 08026A 21059.37713407 -.00000005 00000-0 17710-4 0 9998
2 32958 98.4380 38.2358 0008009 321.6273 38.4333 14.18648537661005
| Epoch (UTC): | 28 February 2021 09:03:04 |
| Eccentricity: | 0.0008009 |
| inclination: | 98.4380° |
| perigee height: | 824 km |
| apogee height: | 836 km |
| right ascension of ascending node: | 38.2358° |
| argument of perigee: | 321.6273° |
| revolutions per day: | 14.18648537 |
| mean anomaly at epoch: | 38.4333° |
| orbit number at epoch: | 66100 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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