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 877U 64053B 23152.17158239 .00000294 00000-0 83785-4 0 9999
2 877 65.0788 56.0266 0074419 324.2521 35.3608 14.59851129118917
Epoch (UTC): | 01 June 2023 04:07:04 |
Eccentricity: | 0.0074419 |
inclination: | 65.0788° |
perigee height: | 641 km |
apogee height: | 746 km |
right ascension of ascending node: | 56.0266° |
argument of perigee: | 324.2521° |
revolutions per day: | 14.59851129 |
mean anomaly at epoch: | 35.3608° |
orbit number at epoch: | 11891 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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