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 00005U 58002B 23038.32239509 .00000137 00000-0 18911-3 0 9993
2 00005 34.2446 135.5714 1845508 14.8362 349.9679 10.85058202310058
| Epoch (UTC): | 07 February 2023 07:44:14 |
| Eccentricity: | 0.1845508 |
| inclination: | 34.2446° |
| perigee height: | 650 km |
| apogee height: | 3831 km |
| right ascension of ascending node: | 135.5714° |
| argument of perigee: | 14.8362° |
| revolutions per day: | 10.85058202 |
| mean anomaly at epoch: | 349.9679° |
| orbit number at epoch: | 31005 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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