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 27607U 02058C 23338.71910758 .00002818 00000-0 40090-3 0 9999
2 27607 64.5551 101.8736 0048887 186.2295 173.8207 14.78024330127420
Epoch (UTC): | 04 December 2023 17:15:30 |
Eccentricity: | 0.0048887 |
inclination: | 64.5551° |
perigee height: | 601 km |
apogee height: | 670 km |
right ascension of ascending node: | 101.8736° |
argument of perigee: | 186.2295° |
revolutions per day: | 14.78024330 |
mean anomaly at epoch: | 173.8207° |
orbit number at epoch: | 12742 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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