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 20401U 90001A 21025.51765811 .00000064 00000-0 00000+0 0 9990
2 20401 13.2388 1.7748 0013292 288.8921 85.9235 0.98995028109389
| Epoch (UTC): | 25 January 2021 12:25:25 |
| Eccentricity: | 0.0013292 |
| inclination: | 13.2388° |
| perigee height: | 36091 km |
| apogee height: | 36204 km |
| right ascension of ascending node: | 1.7748° |
| argument of perigee: | 288.8921° |
| revolutions per day: | 0.98995028 |
| mean anomaly at epoch: | 85.9235° |
| orbit number at epoch: | 10938 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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