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 31232U 99025BLN 22265.49374580 .00004595 00000-0 19044-2 0 9996
2 31232 98.9995 5.5779 0041630 182.8181 177.2770 14.26591299798988
Epoch (UTC): | 22 September 2022 11:50:59 |
Eccentricity: | 0.0041630 |
inclination: | 98.9995° |
perigee height: | 773 km |
apogee height: | 833 km |
right ascension of ascending node: | 5.5779° |
argument of perigee: | 182.8181° |
revolutions per day: | 14.26591299 |
mean anomaly at epoch: | 177.2770° |
orbit number at epoch: | 79898 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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