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 38212U 93036BTC 24355.60055272 .00004793 00000-0 66901-3 0 9991
2 38212 74.0525 55.2903 0099274 217.5273 141.8945 14.74577678763287
Epoch (UTC): | 20 December 2024 14:24:47 |
Eccentricity: | 0.0099274 |
inclination: | 74.0525° |
perigee height: | 577 km |
apogee height: | 716 km |
right ascension of ascending node: | 55.2903° |
argument of perigee: | 217.5273° |
revolutions per day: | 14.74577678 |
mean anomaly at epoch: | 141.8945° |
orbit number at epoch: | 76328 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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