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 19649U 88102A 23150.42814537 .00000137 00000-0 95580-4 0 9995
2 19649 70.9984 184.1263 0007511 255.3022 104.7268 14.14836483781664
Epoch (UTC): | 30 May 2023 10:16:31 |
Eccentricity: | 0.0007511 |
inclination: | 70.9984° |
perigee height: | 837 km |
apogee height: | 848 km |
right ascension of ascending node: | 184.1263° |
argument of perigee: | 255.3022° |
revolutions per day: | 14.14836483 |
mean anomaly at epoch: | 104.7268° |
orbit number at epoch: | 78166 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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