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 00053U 60009E 21102.25797915 -.00000024 00000-0 58686-3 0 9997
2 00053 47.2779 57.5151 0099102 245.2579 113.7870 12.17254661704963
Epoch (UTC): | 12 April 2021 06:11:29 |
Eccentricity: | 0.0099102 |
inclination: | 47.2779° |
perigee height: | 1525 km |
apogee height: | 1683 km |
right ascension of ascending node: | 57.5151° |
argument of perigee: | 245.2579° |
revolutions per day: | 12.17254661 |
mean anomaly at epoch: | 113.7870° |
orbit number at epoch: | 70496 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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