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 28097U 03054C 19329.72460655 0.00000000 00000-0 00000-0 0 00
2 28097 63.4076 201.3406 0381192 358.8607 1.1393 13.40758872 03
Epoch (UTC): | 25 November 2019 17:23:26 |
Eccentricity: | 0.0381192 |
inclination: | 63.4076° |
perigee height: | 821 km |
apogee height: | 1392 km |
right ascension of ascending node: | 201.3406° |
argument of perigee: | 358.8607° |
revolutions per day: | 13.40758872 |
mean anomaly at epoch: | 1.1393° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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