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 12904U 81103B 21018.79595545 -.00000172 00000-0 -13343-4 0 9990
2 12904 81.1748 216.8162 0029446 68.4061 292.0295 15.05919299690186
Epoch (UTC): | 18 January 2021 19:06:10 |
Eccentricity: | 0.0029446 |
inclination: | 81.1748° |
perigee height: | 528 km |
apogee height: | 569 km |
right ascension of ascending node: | 216.8162° |
argument of perigee: | 68.4061° |
revolutions per day: | 15.05919299 |
mean anomaly at epoch: | 292.0295° |
orbit number at epoch: | 69018 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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