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 15369U 84111A 23149.77671535 .00007129 00000-0 29619-3 0 9998
2 15369 82.5234 139.8001 0012224 265.1769 94.8072 15.23578250109894
Epoch (UTC): | 29 May 2023 18:38:28 |
Eccentricity: | 0.0012224 |
inclination: | 82.5234° |
perigee height: | 486 km |
apogee height: | 503 km |
right ascension of ascending node: | 139.8001° |
argument of perigee: | 265.1769° |
revolutions per day: | 15.23578250 |
mean anomaly at epoch: | 94.8072° |
orbit number at epoch: | 10989 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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