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 40025U 14033R 22229.07497596 .00001617 00000-0 17050-3 0 9997
2 40025 97.9612 166.9599 0011160 211.5152 148.5398 14.90713285443300
Epoch (UTC): | 17 August 2022 01:47:57 |
Eccentricity: | 0.0011160 |
inclination: | 97.9612° |
perigee height: | 588 km |
apogee height: | 603 km |
right ascension of ascending node: | 166.9599° |
argument of perigee: | 211.5152° |
revolutions per day: | 14.90713285 |
mean anomaly at epoch: | 148.5398° |
orbit number at epoch: | 44330 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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