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 20641U 90050A 22276.67374687 0.00000000 00000-0 00000-0 0 07
2 20641 63.4556 128.1917 4047676 265.2311 48.6901 6.02594065 02
| Epoch (UTC): | 03 October 2022 16:10:11 |
| Eccentricity: | 0.4047676 |
| inclination: | 63.4556° |
| perigee height: | 1215 km |
| apogee height: | 11541 km |
| right ascension of ascending node: | 128.1917° |
| argument of perigee: | 265.2311° |
| revolutions per day: | 6.02594065 |
| mean anomaly at epoch: | 48.6901° |
| 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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