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 23150.81763547 .00002821 00000-0 20449-3 0 9996
2 29507 97.6891 184.1380 0045116 137.9680 222.5022 15.03953742907034
| Epoch (UTC): | 30 May 2023 19:37:23 |
| Eccentricity: | 0.0045116 |
| inclination: | 97.6891° |
| perigee height: | 523 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 184.1380° |
| argument of perigee: | 137.9680° |
| revolutions per day: | 15.03953742 |
| mean anomaly at epoch: | 222.5022° |
| orbit number at epoch: | 90703 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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