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 37364U 11006A 22179.89878750 0.00000000 00000-0 00000-0 0 07
2 37364 90.1637 64.7658 0019235 117.4818 242.3351 13.11794307 03
Epoch (UTC): | 28 June 2022 21:34:15 |
Eccentricity: | 0.0019235 |
inclination: | 90.1637° |
perigee height: | 1201 km |
apogee height: | 1231 km |
right ascension of ascending node: | 64.7658° |
argument of perigee: | 117.4818° |
revolutions per day: | 13.11794307 |
mean anomaly at epoch: | 242.3351° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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