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 12389U 81033B 15192.92184244 .24045308 -12285-5 13476-3 0 9994
2 12389 082.8246 077.2321 0005162 254.4661 106.7109 16.55182833770380
Epoch (UTC): | 11 July 2015 22:07:27 |
Eccentricity: | 0.0005162 |
inclination: | 82.8246° |
perigee height: | 122 km |
apogee height: | 129 km |
right ascension of ascending node: | 77.2321° |
argument of perigee: | 254.4661° |
revolutions per day: | 16.55182833 |
mean anomaly at epoch: | 106.7109° |
orbit number at epoch: | 77038 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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