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 37057U 99025EER 22176.34215233 .00000100 00000-0 76886-4 0 9998
2 37057 99.0306 208.4312 0292196 16.4892 344.5532 13.93562579459453
Epoch (UTC): | 25 June 2022 08:12:41 |
Eccentricity: | 0.0292196 |
inclination: | 99.0306° |
perigee height: | 703 km |
apogee height: | 1129 km |
right ascension of ascending node: | 208.4312° |
argument of perigee: | 16.4892° |
revolutions per day: | 13.93562579 |
mean anomaly at epoch: | 344.5532° |
orbit number at epoch: | 45945 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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