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 25336U 98029A 20265.05097588 0.00000000 00000-0 00000-0 0 07
2 25336 8.3875 352.4651 0040444 286.7476 72.8143 1.00270000 09
Epoch (UTC): | 21 September 2020 01:13:24 |
Eccentricity: | 0.0040444 |
inclination: | 8.3875° |
perigee height: | 35616 km |
apogee height: | 35957 km |
right ascension of ascending node: | 352.4651° |
argument of perigee: | 286.7476° |
revolutions per day: | 1.00270000 |
mean anomaly at epoch: | 72.8143° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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