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 33066U 08031G 24281.53417564 .00003362 00000-0 56477-3 0 9998
2 33066 48.4408 215.8416 0007648 248.1402 111.8697 14.71721271875456
Epoch (UTC): | 07 October 2024 12:49:12 |
Eccentricity: | 0.0007648 |
inclination: | 48.4408° |
perigee height: | 650 km |
apogee height: | 661 km |
right ascension of ascending node: | 215.8416° |
argument of perigee: | 248.1402° |
revolutions per day: | 14.71721271 |
mean anomaly at epoch: | 111.8697° |
orbit number at epoch: | 87545 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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