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 33994U 93036GD 24357.82539155 .00000679 00000-0 21957-3 0 9997
2 33994 74.0431 127.0192 0023508 348.8176 132.4794 14.40841604833079
Epoch (UTC): | 22 December 2024 19:48:33 |
Eccentricity: | 0.0023508 |
inclination: | 74.0431° |
perigee height: | 739 km |
apogee height: | 772 km |
right ascension of ascending node: | 127.0192° |
argument of perigee: | 348.8176° |
revolutions per day: | 14.40841604 |
mean anomaly at epoch: | 132.4794° |
orbit number at epoch: | 83307 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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