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 15944U 85069A 23027.34353453 .00009812 00000-0 39188-3 0 9997
2 15944 82.5071 352.9859 0015273 169.8033 190.3517 15.24897696 49205
Epoch (UTC): | 27 January 2023 08:14:41 |
Eccentricity: | 0.0015273 |
inclination: | 82.5071° |
perigee height: | 480 km |
apogee height: | 501 km |
right ascension of ascending node: | 352.9859° |
argument of perigee: | 169.8033° |
revolutions per day: | 15.24897696 |
mean anomaly at epoch: | 190.3517° |
orbit number at epoch: | 4920 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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