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 23190U 94045B 23156.90868118 -.00000002 00000-0 21317-4 0 9996
2 23190 74.0294 90.3327 0019915 298.8249 61.0871 13.74174068446372
Epoch (UTC): | 05 June 2023 21:48:30 |
Eccentricity: | 0.0019915 |
inclination: | 74.0294° |
perigee height: | 970 km |
apogee height: | 999 km |
right ascension of ascending node: | 90.3327° |
argument of perigee: | 298.8249° |
revolutions per day: | 13.74174068 |
mean anomaly at epoch: | 61.0871° |
orbit number at epoch: | 44637 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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