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 37162U 10046A 23080.88693828 0.00000000 00000-0 00000-0 0 08
2 37162 122.9992 223.9918 0008793 171.6307 188.4265 13.41437399 09
Epoch (UTC): | 21 March 2023 21:17:11 |
Eccentricity: | 0.0008793 |
inclination: | 122.9992° |
perigee height: | 1097 km |
apogee height: | 1110 km |
right ascension of ascending node: | 223.9918° |
argument of perigee: | 171.6307° |
revolutions per day: | 13.41437399 |
mean anomaly at epoch: | 188.4265° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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