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 16613U 86019A 23152.15210674 .00000839 00000-0 14145-3 0 9998
2 16613 98.7509 359.6208 0140996 134.8532 226.4227 14.66182404647979
Epoch (UTC): | 01 June 2023 03:39:02 |
Eccentricity: | 0.0140996 |
inclination: | 98.7509° |
perigee height: | 574 km |
apogee height: | 773 km |
right ascension of ascending node: | 359.6208° |
argument of perigee: | 134.8532° |
revolutions per day: | 14.66182404 |
mean anomaly at epoch: | 226.4227° |
orbit number at epoch: | 64797 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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