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 5435U 71071A 18115.90350429 -.00000035 +00000-0 +35512-4 0 9990
2 5435 050.1409 272.9355 0110679 162.1342 198.3525 14.55097250442476
Epoch (UTC): | 25 April 2018 21:41:02 |
Eccentricity: | 0.0110679 |
inclination: | 50.1409° |
perigee height: | 630 km |
apogee height: | 787 km |
right ascension of ascending node: | 272.9355° |
argument of perigee: | 162.1342° |
revolutions per day: | 14.55097250 |
mean anomaly at epoch: | 198.3525° |
orbit number at epoch: | 44247 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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