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 17974U 87041B 23156.61187247 .00000212 00000-0 12811-3 0 9992
2 17974 71.0084 357.7150 0015648 300.4487 115.9205 14.17359860865239
Epoch (UTC): | 05 June 2023 14:41:05 |
Eccentricity: | 0.0015648 |
inclination: | 71.0084° |
perigee height: | 823 km |
apogee height: | 845 km |
right ascension of ascending node: | 357.7150° |
argument of perigee: | 300.4487° |
revolutions per day: | 14.17359860 |
mean anomaly at epoch: | 115.9205° |
orbit number at epoch: | 86523 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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