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 42778U 17036P 23333.08702942 .00049219 00000-0 88257-3 0 9999
2 42778 97.1322 4.9361 0005195 202.2391 157.8636 15.49765921358164
Epoch (UTC): | 29 November 2023 02:05:19 |
Eccentricity: | 0.0005195 |
inclination: | 97.1322° |
perigee height: | 414 km |
apogee height: | 421 km |
right ascension of ascending node: | 4.9361° |
argument of perigee: | 202.2391° |
revolutions per day: | 15.49765921 |
mean anomaly at epoch: | 157.8636° |
orbit number at epoch: | 35816 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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