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 23157.07167533 .00002916 00000-0 21097-3 0 9999
2 29507 97.6869 190.3566 0045361 117.6535 242.9306 15.03993402908028
| Epoch (UTC): | 06 June 2023 01:43:12 |
| Eccentricity: | 0.0045361 |
| inclination: | 97.6869° |
| perigee height: | 523 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 190.3566° |
| argument of perigee: | 117.6535° |
| revolutions per day: | 15.03993402 |
| mean anomaly at epoch: | 242.9306° |
| orbit number at epoch: | 90802 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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