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 09013U 76067B 22222.26469096 -.00000082 00000-0 -94779-4 0 9993
2 09013 65.8674 316.1093 0707200 56.3338 310.3069 12.35349494 78526
Epoch (UTC): | 10 August 2022 06:21:09 |
Eccentricity: | 0.0707200 |
inclination: | 65.8674° |
perigee height: | 967 km |
apogee height: | 2085 km |
right ascension of ascending node: | 316.1093° |
argument of perigee: | 56.3338° |
revolutions per day: | 12.35349494 |
mean anomaly at epoch: | 310.3069° |
orbit number at epoch: | 7852 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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