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 39416U 13066A 23336.86117691 .00003441 00000-0 39070-3 0 9999
2 39416 97.6449 298.1497 0040543 41.6525 318.7767 14.86340538543219
Epoch (UTC): | 02 December 2023 20:40:05 |
Eccentricity: | 0.0040543 |
inclination: | 97.6449° |
perigee height: | 581 km |
apogee height: | 638 km |
right ascension of ascending node: | 298.1497° |
argument of perigee: | 41.6525° |
revolutions per day: | 14.86340538 |
mean anomaly at epoch: | 318.7767° |
orbit number at epoch: | 54321 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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