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 26931U 01043C 23038.74965622 .00000360 00000-0 16854-3 0 9992
2 26931 67.0509 171.0178 0005921 282.6217 77.4222 14.30812884115066
Epoch (UTC): | 07 February 2023 17:59:30 |
Eccentricity: | 0.0005921 |
inclination: | 67.0509° |
perigee height: | 785 km |
apogee height: | 793 km |
right ascension of ascending node: | 171.0178° |
argument of perigee: | 282.6217° |
revolutions per day: | 14.30812884 |
mean anomaly at epoch: | 77.4222° |
orbit number at epoch: | 11506 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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