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 43729U 18096L 22176.79409192 .00017467 00000-0 45900-3 0 9994
2 43729 97.3581 259.8415 0013428 31.3423 328.8620 15.38571765199420
Epoch (UTC): | 25 June 2022 19:03:29 |
Eccentricity: | 0.0013428 |
inclination: | 97.3581° |
perigee height: | 441 km |
apogee height: | 459 km |
right ascension of ascending node: | 259.8415° |
argument of perigee: | 31.3423° |
revolutions per day: | 15.38571765 |
mean anomaly at epoch: | 328.8620° |
orbit number at epoch: | 19942 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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