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 22739U 93050A 23275.42599156 .00000286 00000-0 17550-3 0 9997
2 22739 98.5669 238.3339 0010620 74.3770 285.8574 14.13050999553942
Epoch (UTC): | 02 October 2023 10:13:25 |
Eccentricity: | 0.0010620 |
inclination: | 98.5669° |
perigee height: | 841 km |
apogee height: | 856 km |
right ascension of ascending node: | 238.3339° |
argument of perigee: | 74.3770° |
revolutions per day: | 14.13050999 |
mean anomaly at epoch: | 285.8574° |
orbit number at epoch: | 55394 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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