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 39770U 14029E 23081.32990161 .00025924 00000-0 21892-2 0 9993
2 39770 97.9580 206.3904 0009162 242.3191 117.7077 14.98051796479134
Epoch (UTC): | 22 March 2023 07:55:03 |
Eccentricity: | 0.0009162 |
inclination: | 97.9580° |
perigee height: | 566 km |
apogee height: | 579 km |
right ascension of ascending node: | 206.3904° |
argument of perigee: | 242.3191° |
revolutions per day: | 14.98051796 |
mean anomaly at epoch: | 117.7077° |
orbit number at epoch: | 47913 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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