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 59U 60013B 19345.65668035 +.00000070 +00000-0 -24168-4 0 9998
2 59 028.2476 108.0030 0189083 141.5561 219.8621 13.52972208921010
Epoch (UTC): | 11 December 2019 15:45:37 |
Eccentricity: | 0.0189083 |
inclination: | 28.2476° |
perigee height: | 920 km |
apogee height: | 1202 km |
right ascension of ascending node: | 108.0030° |
argument of perigee: | 141.5561° |
revolutions per day: | 13.52972208 |
mean anomaly at epoch: | 219.8621° |
orbit number at epoch: | 92101 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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