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 32789U 08021G 19341.71113684 .00000588 00000-0 42938-4 0 9990
2 32789 97.4445 26.0204 0010668 254.0739 105.9314 15.07306600632876
Epoch (UTC): | 07 December 2019 17:04:02 |
Eccentricity: | 0.0010668 |
inclination: | 97.4445° |
perigee height: | 537 km |
apogee height: | 552 km |
right ascension of ascending node: | 26.0204° |
argument of perigee: | 254.0739° |
revolutions per day: | 15.07306600 |
mean anomaly at epoch: | 105.9314° |
orbit number at epoch: | 63287 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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