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 40903U 15049E 22142.10307697 .00030934 00000-0 50641-3 0 9997
2 40903 97.1805 200.6145 0009592 205.8499 210.1430 15.52395838375171
Epoch (UTC): | 22 May 2022 02:28:25 |
Eccentricity: | 0.0009592 |
inclination: | 97.1805° |
perigee height: | 403 km |
apogee height: | 416 km |
right ascension of ascending node: | 200.6145° |
argument of perigee: | 205.8499° |
revolutions per day: | 15.52395838 |
mean anomaly at epoch: | 210.1430° |
orbit number at epoch: | 37517 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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