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 23086.61692951 .02979572 15726-1 27504-2 0 9993
2 40900 97.3468 116.4761 0007272 233.4772 247.8234 16.15227161418469
Epoch (UTC): | 27 March 2023 14:48:22 |
Eccentricity: | 0.0007272 |
inclination: | 97.3468° |
perigee height: | 228 km |
apogee height: | 237 km |
right ascension of ascending node: | 116.4761° |
argument of perigee: | 233.4772° |
revolutions per day: | 16.15227161 |
mean anomaly at epoch: | 247.8234° |
orbit number at epoch: | 41846 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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