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 42761U 17034D 22181.63753109 .00002324 00000-0 14543-3 0 9994
2 42761 43.0180 258.8020 0009467 6.3293 143.3249 15.12086054278355
Epoch (UTC): | 30 June 2022 15:18:02 |
Eccentricity: | 0.0009467 |
inclination: | 43.0180° |
perigee height: | 523 km |
apogee height: | 536 km |
right ascension of ascending node: | 258.8020° |
argument of perigee: | 6.3293° |
revolutions per day: | 15.12086054 |
mean anomaly at epoch: | 143.3249° |
orbit number at epoch: | 27835 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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