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 23331.04346321 .00000443 00000-0 53955-3 0 9996
2 00005 34.2598 313.3424 1843308 252.7295 86.4146 10.85118526341854
| Epoch (UTC): | 27 November 2023 01:02:35 |
| Eccentricity: | 0.1843308 |
| inclination: | 34.2598° |
| perigee height: | 651 km |
| apogee height: | 3828 km |
| right ascension of ascending node: | 313.3424° |
| argument of perigee: | 252.7295° |
| revolutions per day: | 10.85118526 |
| mean anomaly at epoch: | 86.4146° |
| orbit number at epoch: | 34185 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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