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 38995U 12063A 23081.70569199 -.00000156 00000-0 00000+0 0 9998
2 38995 65.3320 140.7573 6826601 242.8910 36.3874 2.00696620 75821
Epoch (UTC): | 22 March 2023 16:56:11 |
Eccentricity: | 0.6826601 |
inclination: | 65.3320° |
perigee height: | 2047 km |
apogee height: | 38294 km |
right ascension of ascending node: | 140.7573° |
argument of perigee: | 242.8910° |
revolutions per day: | 2.00696620 |
mean anomaly at epoch: | 36.3874° |
orbit number at epoch: | 7582 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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