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 4071U 69070B 23338.31521496 .00001585 00000-0 30716-3 0 9993
2 4071 74.0487 277.8040 0013968 3.7584 356.3686 14.64109299883142
Epoch (UTC): | 04 December 2023 07:33:54 |
Eccentricity: | 0.0013968 |
inclination: | 74.0487° |
perigee height: | 670 km |
apogee height: | 690 km |
right ascension of ascending node: | 277.8040° |
argument of perigee: | 3.7584° |
revolutions per day: | 14.64109299 |
mean anomaly at epoch: | 356.3686° |
orbit number at epoch: | 88314 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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