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 42000U 17008BE 21023.16833244 .00001001 00000-0 42957-4 0 9994
2 42000 97.3288 89.7695 0006671 263.9095 96.1382 15.24972536218243
Epoch (UTC): | 23 January 2021 04:02:23 |
Eccentricity: | 0.0006671 |
inclination: | 97.3288° |
perigee height: | 486 km |
apogee height: | 495 km |
right ascension of ascending node: | 89.7695° |
argument of perigee: | 263.9095° |
revolutions per day: | 15.24972536 |
mean anomaly at epoch: | 96.1382° |
orbit number at epoch: | 21824 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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