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 29507U 06046C 23153.81161255 .00003361 00000-0 24258-3 0 9999
2 29507 97.6881 187.1149 0045362 128.1027 232.4303 15.03974401907485
| Epoch (UTC): | 02 June 2023 19:28:43 |
| Eccentricity: | 0.0045362 |
| inclination: | 97.6881° |
| perigee height: | 523 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 187.1149° |
| argument of perigee: | 128.1027° |
| revolutions per day: | 15.03974401 |
| mean anomaly at epoch: | 232.4303° |
| orbit number at epoch: | 90748 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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