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 25544U 98067A 23028.52354167 .00020920 00000-0 37018-3 0 9993
2 25544 51.6439 300.3153 0004951 283.6316 84.5269 15.50251265380134
Epoch (UTC): | 28 January 2023 12:33:54 |
Eccentricity: | 0.0004951 |
inclination: | 51.6439° |
perigee height: | 412 km |
apogee height: | 419 km |
right ascension of ascending node: | 300.3153° |
argument of perigee: | 283.6316° |
revolutions per day: | 15.50251265 |
mean anomaly at epoch: | 84.5269° |
orbit number at epoch: | 38013 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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