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 26635U 00080A 20176.02205115 0.00000000 00000-0 00000-0 0 05
2 26635 9.0982 30.6186 0007738 181.7318 178.2784 1.00270000 07
| Epoch (UTC): | 24 June 2020 00:31:45 |
| Eccentricity: | 0.0007738 |
| inclination: | 9.0982° |
| perigee height: | 35754 km |
| apogee height: | 35819 km |
| right ascension of ascending node: | 30.6186° |
| argument of perigee: | 181.7318° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 178.2784° |
| 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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