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 12U 59001B 19321.61423685 +.00000048 +00000-0 +33963-4 0 9999
2 12 032.9015 015.6144 1666066 036.9546 333.4957 11.44314864255596
| Epoch (UTC): | 17 November 2019 14:44:30 |
| Eccentricity: | 0.1666066 |
| inclination: | 32.9015° |
| perigee height: | 554 km |
| apogee height: | 3326 km |
| right ascension of ascending node: | 15.6144° |
| argument of perigee: | 36.9546° |
| revolutions per day: | 11.44314864 |
| mean anomaly at epoch: | 333.4957° |
| orbit number at epoch: | 25559 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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