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 33493U 09002B 22178.55204143 .00002864 00000-0 23586-3 0 9994
2 33493 98.2250 165.6977 0016129 136.4985 223.7512 14.99880595730499
Epoch (UTC): | 27 June 2022 13:14:56 |
Eccentricity: | 0.0016129 |
inclination: | 98.2250° |
perigee height: | 556 km |
apogee height: | 578 km |
right ascension of ascending node: | 165.6977° |
argument of perigee: | 136.4985° |
revolutions per day: | 14.99880595 |
mean anomaly at epoch: | 223.7512° |
orbit number at epoch: | 73049 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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