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 38770U 12048N 23133.89531280 0.00009000 00000-0 48901-3 0 05
2 38770 64.6522 44.0178 0134320 171.2802 188.7198 15.06729597 03
Epoch (UTC): | 13 May 2023 21:29:15 |
Eccentricity: | 0.0134320 |
inclination: | 64.6522° |
perigee height: | 453 km |
apogee height: | 639 km |
right ascension of ascending node: | 44.0178° |
argument of perigee: | 171.2802° |
revolutions per day: | 15.06729597 |
mean anomaly at epoch: | 188.7198° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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