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 33499U 09002H 23080.93242029 .00002093 00000-0 30608-3 0 9997
2 33499 98.1844 332.1011 0009592 139.8731 220.3188 14.76755627761189
Epoch (UTC): | 21 March 2023 22:22:41 |
Eccentricity: | 0.0009592 |
inclination: | 98.1844° |
perigee height: | 633 km |
apogee height: | 646 km |
right ascension of ascending node: | 332.1011° |
argument of perigee: | 139.8731° |
revolutions per day: | 14.76755627 |
mean anomaly at epoch: | 220.3188° |
orbit number at epoch: | 76118 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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