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 28773U 05025A 21023.20533578 .00001112 00000-0 49026-4 0 9990
2 28773 31.3829 27.3469 0004635 259.1445 100.8681 15.18028643857354
Epoch (UTC): | 23 January 2021 04:55:41 |
Eccentricity: | 0.0004635 |
inclination: | 31.3829° |
perigee height: | 508 km |
apogee height: | 515 km |
right ascension of ascending node: | 27.3469° |
argument of perigee: | 259.1445° |
revolutions per day: | 15.18028643 |
mean anomaly at epoch: | 100.8681° |
orbit number at epoch: | 85735 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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