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 29712U 07001D 23016.55835740 .52449672 27118-5 15003-2 0 9992
2 29712 97.3306 56.4390 0007030 254.9982 252.9779 16.44974694877464
Epoch (UTC): | 16 January 2023 13:24:02 |
Eccentricity: | 0.0007030 |
inclination: | 97.3306° |
perigee height: | 148 km |
apogee height: | 157 km |
right ascension of ascending node: | 56.4390° |
argument of perigee: | 254.9982° |
revolutions per day: | 16.44974694 |
mean anomaly at epoch: | 252.9779° |
orbit number at epoch: | 87746 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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