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 13354U 82069B 23150.80107429 .00000174 00000-0 15343-3 0 9994
2 13354 82.9582 164.1593 0052809 143.7008 216.7752 13.79027263 57347
Epoch (UTC): | 30 May 2023 19:13:32 |
Eccentricity: | 0.0052809 |
inclination: | 82.9582° |
perigee height: | 928 km |
apogee height: | 1006 km |
right ascension of ascending node: | 164.1593° |
argument of perigee: | 143.7008° |
revolutions per day: | 13.79027263 |
mean anomaly at epoch: | 216.7752° |
orbit number at epoch: | 5734 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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