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 23341.16978469 .00000296 00000-0 36262-3 0 9992
2 00005 34.2579 282.1504 1842730 298.2933 44.3888 10.85129027342953
| Epoch (UTC): | 07 December 2023 04:04:29 |
| Eccentricity: | 0.1842730 |
| inclination: | 34.2579° |
| perigee height: | 652 km |
| apogee height: | 3828 km |
| right ascension of ascending node: | 282.1504° |
| argument of perigee: | 298.2933° |
| revolutions per day: | 10.85129027 |
| mean anomaly at epoch: | 44.3888° |
| orbit number at epoch: | 34295 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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