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 39090U 13009E 24308.75064389 .00002018 00000-0 70303-3 0 9990
2 39090 98.3786 133.2391 0008523 189.0884 171.0150 14.36419272612296
Epoch (UTC): | 03 November 2024 18:00:55 |
Eccentricity: | 0.0008523 |
inclination: | 98.3786° |
perigee height: | 764 km |
apogee height: | 776 km |
right ascension of ascending node: | 133.2391° |
argument of perigee: | 189.0884° |
revolutions per day: | 14.36419272 |
mean anomaly at epoch: | 171.0150° |
orbit number at epoch: | 61229 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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