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 39430U 13066Q 23338.16336745 .00002725 00000-0 46812-3 0 9999
2 39430 97.7561 219.2781 0143563 154.5802 206.2554 14.62840503534372
Epoch (UTC): | 04 December 2023 03:55:14 |
Eccentricity: | 0.0143563 |
inclination: | 97.7561° |
perigee height: | 582 km |
apogee height: | 785 km |
right ascension of ascending node: | 219.2781° |
argument of perigee: | 154.5802° |
revolutions per day: | 14.62840503 |
mean anomaly at epoch: | 206.2554° |
orbit number at epoch: | 53437 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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