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 23160.66434388 .00002949 00000-0 21323-3 0 9991
2 29507 97.6860 193.9283 0045111 106.0759 254.5441 15.04015512908563
| Epoch (UTC): | 09 June 2023 15:56:39 |
| Eccentricity: | 0.0045111 |
| inclination: | 97.6860° |
| perigee height: | 523 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 193.9283° |
| argument of perigee: | 106.0759° |
| revolutions per day: | 15.04015512 |
| mean anomaly at epoch: | 254.5441° |
| orbit number at epoch: | 90856 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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