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 27844U 03031E 24306.93592185 .00001874 00000-0 84126-3 0 9993
2 27844 98.6789 312.0908 0010805 103.2325 257.0060 14.23597814107380
Epoch (UTC): | 01 November 2024 22:27:43 |
Eccentricity: | 0.0010805 |
inclination: | 98.6789° |
perigee height: | 805 km |
apogee height: | 821 km |
right ascension of ascending node: | 312.0908° |
argument of perigee: | 103.2325° |
revolutions per day: | 14.23597814 |
mean anomaly at epoch: | 257.0060° |
orbit number at epoch: | 10738 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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