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 39929U 94029AGC 24276.16362709 .00014782 00000-0 28586-2 0 9994
2 39929 81.9433 72.4878 0261573 273.6895 83.4423 14.43697581540711
Epoch (UTC): | 02 October 2024 03:55:37 |
Eccentricity: | 0.0261573 |
inclination: | 81.9433° |
perigee height: | 560 km |
apogee height: | 932 km |
right ascension of ascending node: | 72.4878° |
argument of perigee: | 273.6895° |
revolutions per day: | 14.43697581 |
mean anomaly at epoch: | 83.4423° |
orbit number at epoch: | 54071 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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