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 42784U 17036V 23088.82906352 .00049829 00000-0 12126-2 0 9994
2 42784 97.1601 127.5318 0007873 37.6256 322.5541 15.40760395320739
Epoch (UTC): | 29 March 2023 19:53:51 |
Eccentricity: | 0.0007873 |
inclination: | 97.1601° |
perigee height: | 438 km |
apogee height: | 449 km |
right ascension of ascending node: | 127.5318° |
argument of perigee: | 37.6256° |
revolutions per day: | 15.40760395 |
mean anomaly at epoch: | 322.5541° |
orbit number at epoch: | 32073 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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