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 35500U 09036C 21026.27846985 .00000028 00000-0 13456-3 0 9993
2 35500 82.4863 230.3515 0006934 120.7361 239.4402 12.41466439523911
Epoch (UTC): | 26 January 2021 06:40:59 |
Eccentricity: | 0.0006934 |
inclination: | 82.4863° |
perigee height: | 1495 km |
apogee height: | 1506 km |
right ascension of ascending node: | 230.3515° |
argument of perigee: | 120.7361° |
revolutions per day: | 12.41466439 |
mean anomaly at epoch: | 239.4402° |
orbit number at epoch: | 52391 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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