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 03890U 69037A 23083.60397322 .00000023 00000-0 11716-3 0 9997
2 03890 99.8422 345.1019 0039138 327.4635 94.1797 13.42572478642353
Epoch (UTC): | 24 March 2023 14:29:43 |
Eccentricity: | 0.0039138 |
inclination: | 99.8422° |
perigee height: | 1070 km |
apogee height: | 1129 km |
right ascension of ascending node: | 345.1019° |
argument of perigee: | 327.4635° |
revolutions per day: | 13.42572478 |
mean anomaly at epoch: | 94.1797° |
orbit number at epoch: | 64235 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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