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 45117U 19071G 22180.52651218 .00016882 00000-0 31680-3 0 9995
2 45117 51.6373 354.7598 0008408 214.7366 145.3074 15.48709580135308
Epoch (UTC): | 29 June 2022 12:38:10 |
Eccentricity: | 0.0008408 |
inclination: | 51.6373° |
perigee height: | 415 km |
apogee height: | 426 km |
right ascension of ascending node: | 354.7598° |
argument of perigee: | 214.7366° |
revolutions per day: | 15.48709580 |
mean anomaly at epoch: | 145.3074° |
orbit number at epoch: | 13530 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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