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 37386U 11014A 23075.98580279 0.00000000 00000-0 00000-0 0 02
2 37386 63.4300 72.6159 0255561 357.4462 2.5538 13.40872496 07
Epoch (UTC): | 16 March 2023 23:39:33 |
Eccentricity: | 0.0255561 |
inclination: | 63.4300° |
perigee height: | 915 km |
apogee height: | 1297 km |
right ascension of ascending node: | 72.6159° |
argument of perigee: | 357.4462° |
revolutions per day: | 13.40872496 |
mean anomaly at epoch: | 2.5538° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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