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 40399U 95015L 22181.54094753 .00000831 00000-0 41163-3 0 9996
2 40399 98.7812 192.9915 0009383 198.3452 161.7387 14.19960795380132
Epoch (UTC): | 30 June 2022 12:58:57 |
Eccentricity: | 0.0009383 |
inclination: | 98.7812° |
perigee height: | 819 km |
apogee height: | 832 km |
right ascension of ascending node: | 192.9915° |
argument of perigee: | 198.3452° |
revolutions per day: | 14.19960795 |
mean anomaly at epoch: | 161.7387° |
orbit number at epoch: | 38013 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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