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 35614U 93036ANH 24358.21759382 .00010720 00000-0 20467-2 0 9990
2 35614 73.9612 292.2428 0085476 228.9882 130.3873 14.61682867826434
Epoch (UTC): | 23 December 2024 05:13:20 |
Eccentricity: | 0.0085476 |
inclination: | 73.9612° |
perigee height: | 627 km |
apogee height: | 748 km |
right ascension of ascending node: | 292.2428° |
argument of perigee: | 228.9882° |
revolutions per day: | 14.61682867 |
mean anomaly at epoch: | 130.3873° |
orbit number at epoch: | 82643 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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