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 42788U 17036Z 19345.70695505 .00001081 00000-0 48443-4 0 9992
2 42788 97.3303 39.9484 0010708 338.2004 21.8776 15.23294683137149
Epoch (UTC): | 11 December 2019 16:58:00 |
Eccentricity: | 0.0010708 |
inclination: | 97.3303° |
perigee height: | 488 km |
apogee height: | 503 km |
right ascension of ascending node: | 39.9484° |
argument of perigee: | 338.2004° |
revolutions per day: | 15.23294683 |
mean anomaly at epoch: | 21.8776° |
orbit number at epoch: | 13714 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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