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 23154.67653165 .00002954 00000-0 21374-3 0 9993
2 29507 97.6878 187.9749 0045395 125.3033 235.2450 15.03979097907667
| Epoch (UTC): | 03 June 2023 16:14:12 |
| Eccentricity: | 0.0045395 |
| inclination: | 97.6878° |
| perigee height: | 523 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 187.9749° |
| argument of perigee: | 125.3033° |
| revolutions per day: | 15.03979097 |
| mean anomaly at epoch: | 235.2450° |
| orbit number at epoch: | 90766 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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