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 39173U 13026B 23037.95355678 -.00000081 00000-0 00000-0 0 9998
2 39173 29.9193 50.8247 7652375 27.1588 357.9300 1.10512640 38693
Epoch (UTC): | 06 February 2023 22:53:07 |
Eccentricity: | 0.7652375 |
inclination: | 29.9193° |
perigee height: | 2899 km |
apogee height: | 63379 km |
right ascension of ascending node: | 50.8247° |
argument of perigee: | 27.1588° |
revolutions per day: | 1.10512640 |
mean anomaly at epoch: | 357.9300° |
orbit number at epoch: | 3869 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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