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 20U 59007A 19320.91801335 +.00000025 +00000-0 -33010-5 0 9998
2 20 033.3489 222.7537 1667083 214.0516 134.1190 11.55691276205898
| Epoch (UTC): | 16 November 2019 22:01:56 |
| Eccentricity: | 0.1667083 |
| inclination: | 33.3489° |
| perigee height: | 508 km |
| apogee height: | 3263 km |
| right ascension of ascending node: | 222.7537° |
| argument of perigee: | 214.0516° |
| revolutions per day: | 11.55691276 |
| mean anomaly at epoch: | 134.1190° |
| orbit number at epoch: | 20589 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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