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 22568U 93014D 22181.78054338 .00000348 00000-0 10595-3 0 9990
2 22568 75.7503 312.9048 0164036 303.8722 220.9895 14.36941528526487
Epoch (UTC): | 30 June 2022 18:43:58 |
Eccentricity: | 0.0164036 |
inclination: | 75.7503° |
perigee height: | 651 km |
apogee height: | 886 km |
right ascension of ascending node: | 312.9048° |
argument of perigee: | 303.8722° |
revolutions per day: | 14.36941528 |
mean anomaly at epoch: | 220.9895° |
orbit number at epoch: | 52648 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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