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 85U 61004C 25126.91579424 .00547528 00000-0 83528-2 0 9990
2 85 38.6281 333.3586 0047038 226.2995 133.3890 15.50513241188530
Epoch (UTC): | 06 May 2025 21:58:44 |
Eccentricity: | 0.0047038 |
inclination: | 38.6281° |
perigee height: | 383 km |
apogee height: | 447 km |
right ascension of ascending node: | 333.3586° |
argument of perigee: | 226.2995° |
revolutions per day: | 15.50513241 |
mean anomaly at epoch: | 133.3890° |
orbit number at epoch: | 18853 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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