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 28654U 05018A 19348.85639977 +.00000100 +00000-0 +79026-4 0 9997
2 28654 099.0726 038.2999 0014697 037.2413 322.9775 14.12474220750719
Epoch (UTC): | 14 December 2019 20:33:12 |
Eccentricity: | 0.0014697 |
inclination: | 99.0726° |
perigee height: | 840 km |
apogee height: | 861 km |
right ascension of ascending node: | 38.2999° |
argument of perigee: | 37.2413° |
revolutions per day: | 14.12474220 |
mean anomaly at epoch: | 322.9775° |
orbit number at epoch: | 75071 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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