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 27561U 02054C 22230.92272958 .00000358 00000-0 91076-4 0 9998
2 27561 98.5091 39.9534 0047056 114.4484 246.1632 14.56131321 47019
Epoch (UTC): | 18 August 2022 22:08:43 |
Eccentricity: | 0.0047056 |
inclination: | 98.5091° |
perigee height: | 672 km |
apogee height: | 739 km |
right ascension of ascending node: | 39.9534° |
argument of perigee: | 114.4484° |
revolutions per day: | 14.56131321 |
mean anomaly at epoch: | 246.1632° |
orbit number at epoch: | 4701 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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