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 15378U 84112A 23150.17780643 -.00000072 00000-0 15147-4 0 9999
2 15378 64.9932 65.3075 0046848 337.4300 22.4699 13.83605496951096
Epoch (UTC): | 30 May 2023 04:16:02 |
Eccentricity: | 0.0046848 |
inclination: | 64.9932° |
perigee height: | 917 km |
apogee height: | 985 km |
right ascension of ascending node: | 65.3075° |
argument of perigee: | 337.4300° |
revolutions per day: | 13.83605496 |
mean anomaly at epoch: | 22.4699° |
orbit number at epoch: | 95109 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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