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 33410U 08053C 25198.49440394 .00004405 00000-0 20346-3 0 9990
2 33410 97.8276 250.2535 0093608 335.1985 24.4762 15.16895984913806
Epoch (UTC): | 17 July 2025 11:51:56 |
Eccentricity: | 0.0093608 |
inclination: | 97.8276° |
perigee height: | 451 km |
apogee height: | 580 km |
right ascension of ascending node: | 250.2535° |
argument of perigee: | 335.1985° |
revolutions per day: | 15.16895984 |
mean anomaly at epoch: | 24.4762° |
orbit number at epoch: | 91380 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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