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 43775U 18099T 25138.58255481 .00003904 00000-0 26682-3 0 9993
2 43775 97.4738 189.6586 0004710 226.8345 133.2489 15.06703038352824
Epoch (UTC): | 18 May 2025 13:58:52 |
Eccentricity: | 0.0004710 |
inclination: | 97.4738° |
perigee height: | 543 km |
apogee height: | 549 km |
right ascension of ascending node: | 189.6586° |
argument of perigee: | 226.8345° |
revolutions per day: | 15.06703038 |
mean anomaly at epoch: | 133.2489° |
orbit number at epoch: | 35282 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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