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 36687U 99025DZH 22216.11342080 .00000212 00000-0 15649-3 0 9990
2 36687 98.6744 337.7854 0094094 105.8967 255.2594 14.03075281455130
Epoch (UTC): | 04 August 2022 02:43:19 |
Eccentricity: | 0.0094094 |
inclination: | 98.6744° |
perigee height: | 815 km |
apogee height: | 951 km |
right ascension of ascending node: | 337.7854° |
argument of perigee: | 105.8967° |
revolutions per day: | 14.03075281 |
mean anomaly at epoch: | 255.2594° |
orbit number at epoch: | 45513 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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