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 36071U 93036AYJ 24358.36247712 .00128554 00000-0 90520-2 0 9995
2 36071 74.0021 13.1640 0008945 282.4226 77.5961 15.04317920823426
Epoch (UTC): | 23 December 2024 08:41:58 |
Eccentricity: | 0.0008945 |
inclination: | 74.0021° |
perigee height: | 547 km |
apogee height: | 560 km |
right ascension of ascending node: | 13.1640° |
argument of perigee: | 282.4226° |
revolutions per day: | 15.04317920 |
mean anomaly at epoch: | 77.5961° |
orbit number at epoch: | 82342 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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