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 31133U 07012R 23342.56372265 .00001585 00000-0 31599-3 0 9990
2 31133 98.3205 294.8476 0076833 324.7938 34.8200 14.61620100885473
Epoch (UTC): | 08 December 2023 13:31:45 |
Eccentricity: | 0.0076833 |
inclination: | 98.3205° |
perigee height: | 633 km |
apogee height: | 742 km |
right ascension of ascending node: | 294.8476° |
argument of perigee: | 324.7938° |
revolutions per day: | 14.61620100 |
mean anomaly at epoch: | 34.8200° |
orbit number at epoch: | 88547 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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