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 22144.88023614 .00000933 00000-0 14896-3 0 9998
2 27607 64.5560 14.0381 0077123 299.0129 60.3260 14.76103380 44894
Epoch (UTC): | 24 May 2022 21:07:32 |
Eccentricity: | 0.0077123 |
inclination: | 64.5560° |
perigee height: | 587 km |
apogee height: | 696 km |
right ascension of ascending node: | 14.0381° |
argument of perigee: | 299.0129° |
revolutions per day: | 14.76103380 |
mean anomaly at epoch: | 60.3260° |
orbit number at epoch: | 4489 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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