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 38254U 12019A 23081.48770184 -.00000172 00000-0 00000+0 0 9998
2 38254 3.9415 62.0007 0003251 283.6889 275.3518 1.00269594 39814
Epoch (UTC): | 22 March 2023 11:42:17 |
Eccentricity: | 0.0003251 |
inclination: | 3.9415° |
perigee height: | 35773 km |
apogee height: | 35800 km |
right ascension of ascending node: | 62.0007° |
argument of perigee: | 283.6889° |
revolutions per day: | 1.00269594 |
mean anomaly at epoch: | 275.3518° |
orbit number at epoch: | 3981 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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