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 25338U 98030A 22137.33922096 .00000236 00000-0 11704-3 0 9997
2 25338 98.6465 167.2779 0010934 34.5906 325.5984 14.26124278248832
Epoch (UTC): | 17 May 2022 08:08:28 |
Eccentricity: | 0.0010934 |
inclination: | 98.6465° |
perigee height: | 797 km |
apogee height: | 812 km |
right ascension of ascending node: | 167.2779° |
argument of perigee: | 34.5906° |
revolutions per day: | 14.26124278 |
mean anomaly at epoch: | 325.5984° |
orbit number at epoch: | 24883 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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