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 33490U 09001A 20325.80395914 0.00000000 00000-0 00000-0 0 03
2 33490 6.0380 33.6616 0007420 291.9043 68.0957 1.00275815 08
| Epoch (UTC): | 20 November 2020 19:17:42 |
| Eccentricity: | 0.0007420 |
| inclination: | 6.0380° |
| perigee height: | 35754 km |
| apogee height: | 35816 km |
| right ascension of ascending node: | 33.6616° |
| argument of perigee: | 291.9043° |
| revolutions per day: | 1.00275815 |
| mean anomaly at epoch: | 68.0957° |
| 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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