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 13066U 82012B 25191.49208894 .00000080 00000-0 65773-4 0 9991
2 13066 82.8967 176.1757 0041996 276.8563 197.4028 13.77358508180364
Epoch (UTC): | 10 July 2025 11:48:36 |
Eccentricity: | 0.0041996 |
inclination: | 82.8967° |
perigee height: | 942 km |
apogee height: | 1004 km |
right ascension of ascending node: | 176.1757° |
argument of perigee: | 276.8563° |
revolutions per day: | 13.77358508 |
mean anomaly at epoch: | 197.4028° |
orbit number at epoch: | 18036 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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