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 21937U 92020A 23083.65469369 .00000095 00000-0 86310-4 0 9995
2 21937 82.9280 268.4419 0033049 193.8107 238.7346 13.73221630550545
Epoch (UTC): | 24 March 2023 15:42:45 |
Eccentricity: | 0.0033049 |
inclination: | 82.9280° |
perigee height: | 963 km |
apogee height: | 1012 km |
right ascension of ascending node: | 268.4419° |
argument of perigee: | 193.8107° |
revolutions per day: | 13.73221630 |
mean anomaly at epoch: | 238.7346° |
orbit number at epoch: | 55054 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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