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 33933U 93036EN 22183.43403723 .00000252 00000-0 10476-3 0 9994
2 33933 74.0887 187.4094 0076082 160.5870 199.8207 14.29692045697662
Epoch (UTC): | 02 July 2022 10:25:00 |
Eccentricity: | 0.0076082 |
inclination: | 74.0887° |
perigee height: | 738 km |
apogee height: | 847 km |
right ascension of ascending node: | 187.4094° |
argument of perigee: | 160.5870° |
revolutions per day: | 14.29692045 |
mean anomaly at epoch: | 199.8207° |
orbit number at epoch: | 69766 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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