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 18748U 88001A 25142.19729986 .00023878 00000-0 40609-3 0 9990
2 18748 82.4562 53.2851 0003430 219.0033 141.0971 15.51278038 45337
Epoch (UTC): | 22 May 2025 04:44:06 |
Eccentricity: | 0.0003430 |
inclination: | 82.4562° |
perigee height: | 410 km |
apogee height: | 415 km |
right ascension of ascending node: | 53.2851° |
argument of perigee: | 219.0033° |
revolutions per day: | 15.51278038 |
mean anomaly at epoch: | 141.0971° |
orbit number at epoch: | 4533 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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