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 20104U 89050B 19321.88661133 +.00000042 +00000-0 +27139-4 0 9993
2 20104 082.9582 235.9518 0042389 229.0902 130.6581 13.77309840526038
| Epoch (UTC): | 17 November 2019 21:16:43 |
| Eccentricity: | 0.0042389 |
| inclination: | 82.9582° |
| perigee height: | 942 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 235.9518° |
| argument of perigee: | 229.0902° |
| revolutions per day: | 13.77309840 |
| mean anomaly at epoch: | 130.6581° |
| orbit number at epoch: | 52603 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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