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 25634U 99008A 23161.28400995 .00000083 00000-0 58531-4 0 9993
2 25634 98.3934 161.8963 0010303 7.7921 352.3414 14.19529431257808
Epoch (UTC): | 10 June 2023 06:48:58 |
Eccentricity: | 0.0010303 |
inclination: | 98.3934° |
perigee height: | 819 km |
apogee height: | 834 km |
right ascension of ascending node: | 161.8963° |
argument of perigee: | 7.7921° |
revolutions per day: | 14.19529431 |
mean anomaly at epoch: | 352.3414° |
orbit number at epoch: | 25780 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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