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 19345.52706605 .00000073 00000-0 64443-4 0 9997
2 28654 99.0733 34.9297 0014813 46.2986 313.9410 14.12473417750348
Epoch (UTC): | 11 December 2019 12:38:58 |
Eccentricity: | 0.0014813 |
inclination: | 99.0733° |
perigee height: | 840 km |
apogee height: | 861 km |
right ascension of ascending node: | 34.9297° |
argument of perigee: | 46.2986° |
revolutions per day: | 14.12473417 |
mean anomaly at epoch: | 313.9410° |
orbit number at epoch: | 75034 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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