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 14700U 84013B 23150.35128054 .00000443 00000-0 50437-4 0 9991
2 14700 82.5358 286.1033 0019598 6.5755 16.4073 14.83829906123151
Epoch (UTC): | 30 May 2023 08:25:50 |
Eccentricity: | 0.0019598 |
inclination: | 82.5358° |
perigee height: | 603 km |
apogee height: | 631 km |
right ascension of ascending node: | 286.1033° |
argument of perigee: | 6.5755° |
revolutions per day: | 14.83829906 |
mean anomaly at epoch: | 16.4073° |
orbit number at epoch: | 12315 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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