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 38734U 12041B 23088.27494474 .00000027 00000-0 11932-3 0 9993
2 38734 82.4708 81.2877 0017679 113.7053 246.5886 12.44840375484428
Epoch (UTC): | 29 March 2023 06:35:55 |
Eccentricity: | 0.0017679 |
inclination: | 82.4708° |
perigee height: | 1472 km |
apogee height: | 1500 km |
right ascension of ascending node: | 81.2877° |
argument of perigee: | 113.7053° |
revolutions per day: | 12.44840375 |
mean anomaly at epoch: | 246.5886° |
orbit number at epoch: | 48442 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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