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 33493U 09002B 22179.48602281 .00002416 00000-0 19976-3 0 9993
2 33493 98.2252 166.6846 0016208 133.6850 226.5718 14.99884626730639
Epoch (UTC): | 28 June 2022 11:39:52 |
Eccentricity: | 0.0016208 |
inclination: | 98.2252° |
perigee height: | 556 km |
apogee height: | 578 km |
right ascension of ascending node: | 166.6846° |
argument of perigee: | 133.6850° |
revolutions per day: | 14.99884626 |
mean anomaly at epoch: | 226.5718° |
orbit number at epoch: | 73063 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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