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 40057U 14034E 23086.14585203 .00006691 00000-0 86648-3 0 9992
2 40057 98.3731 275.5047 0011183 144.0651 216.1285 14.81153821471285
Epoch (UTC): | 27 March 2023 03:30:01 |
Eccentricity: | 0.0011183 |
inclination: | 98.3731° |
perigee height: | 618 km |
apogee height: | 633 km |
right ascension of ascending node: | 275.5047° |
argument of perigee: | 144.0651° |
revolutions per day: | 14.81153821 |
mean anomaly at epoch: | 216.1285° |
orbit number at epoch: | 47128 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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