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 43803U 18099AX 23156.11408502 .00005622 00000-0 44755-3 0 9996
2 43803 97.5694 218.9920 0014030 131.2702 228.9733 15.00699814245889
Epoch (UTC): | 05 June 2023 02:44:16 |
Eccentricity: | 0.0014030 |
inclination: | 97.5694° |
perigee height: | 555 km |
apogee height: | 574 km |
right ascension of ascending node: | 218.9920° |
argument of perigee: | 131.2702° |
revolutions per day: | 15.00699814 |
mean anomaly at epoch: | 228.9733° |
orbit number at epoch: | 24588 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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