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 42017U 17008BX 23158.76512650 .00207145 00000-0 12676-2 0 9994
2 42017 97.2083 229.7088 0002588 203.5571 156.5578 15.76742840351984
Epoch (UTC): | 07 June 2023 18:21:46 |
Eccentricity: | 0.0002588 |
inclination: | 97.2083° |
perigee height: | 338 km |
apogee height: | 341 km |
right ascension of ascending node: | 229.7088° |
argument of perigee: | 203.5571° |
revolutions per day: | 15.76742840 |
mean anomaly at epoch: | 156.5578° |
orbit number at epoch: | 35198 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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