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 11061U 78096B 22228.86939931 .00008279 00000-0 67491-3 0 9999
2 11061 98.8576 314.8240 0002251 354.8822 5.2374 14.99788557324056
Epoch (UTC): | 16 August 2022 20:51:56 |
Eccentricity: | 0.0002251 |
inclination: | 98.8576° |
perigee height: | 566 km |
apogee height: | 569 km |
right ascension of ascending node: | 314.8240° |
argument of perigee: | 354.8822° |
revolutions per day: | 14.99788557 |
mean anomaly at epoch: | 5.2374° |
orbit number at epoch: | 32405 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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