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 27665U 03005C 25197.72931365 -.00000017 00000-0 26788-4 0 9998
2 27665 39.5736 195.8493 0008085 18.1148 149.8077 14.29406423173017
Epoch (UTC): | 16 July 2025 17:30:12 |
Eccentricity: | 0.0008085 |
inclination: | 39.5736° |
perigee height: | 788 km |
apogee height: | 799 km |
right ascension of ascending node: | 195.8493° |
argument of perigee: | 18.1148° |
revolutions per day: | 14.29406423 |
mean anomaly at epoch: | 149.8077° |
orbit number at epoch: | 17301 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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