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 38089U 12007C 22147.46375407 .00003101 00000-0 58196-3 0 9997
2 38089 49.5499 200.5693 5030703 124.7079 293.4498 5.55874517205657
Epoch (UTC): | 27 May 2022 11:07:48 |
Eccentricity: | 0.5030703 |
inclination: | 49.5499° |
perigee height: | 311 km |
apogee height: | 13855 km |
right ascension of ascending node: | 200.5693° |
argument of perigee: | 124.7079° |
revolutions per day: | 5.55874517 |
mean anomaly at epoch: | 293.4498° |
orbit number at epoch: | 20565 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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