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 00020U 59007A 21059.85037666 .00000086 00000-0 25693-4 0 9994
2 00020 33.3485 348.5722 1665924 186.9457 170.4991 11.55800716260276
| Epoch (UTC): | 28 February 2021 20:24:32 |
| Eccentricity: | 0.1665924 |
| inclination: | 33.3485° |
| perigee height: | 508 km |
| apogee height: | 3261 km |
| right ascension of ascending node: | 348.5722° |
| argument of perigee: | 186.9457° |
| revolutions per day: | 11.55800716 |
| mean anomaly at epoch: | 170.4991° |
| orbit number at epoch: | 26027 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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