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 40900U 15049B 19345.80007900 .00001634 00000-0 71659-4 0 9994
2 40900 97.4354 353.4522 0011127 289.8223 243.9002 15.23377883234463
Epoch (UTC): | 11 December 2019 19:12:06 |
Eccentricity: | 0.0011127 |
inclination: | 97.4354° |
perigee height: | 488 km |
apogee height: | 503 km |
right ascension of ascending node: | 353.4522° |
argument of perigee: | 289.8223° |
revolutions per day: | 15.23377883 |
mean anomaly at epoch: | 243.9002° |
orbit number at epoch: | 23446 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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