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 23080.16983201 .00092828 00000-0 13800-2 0 9996
2 42017 97.2253 149.2565 0002050 305.5370 54.5693 15.54845064339690
Epoch (UTC): | 21 March 2023 04:04:33 |
Eccentricity: | 0.0002050 |
inclination: | 97.2253° |
perigee height: | 401 km |
apogee height: | 404 km |
right ascension of ascending node: | 149.2565° |
argument of perigee: | 305.5370° |
revolutions per day: | 15.54845064 |
mean anomaly at epoch: | 54.5693° |
orbit number at epoch: | 33969 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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