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 23150.08576807 .00002703 00000-0 19620-3 0 9994
2 29507 97.6893 183.4103 0045035 140.4009 220.0520 15.03949181906975
| Epoch (UTC): | 30 May 2023 02:03:30 |
| Eccentricity: | 0.0045035 |
| inclination: | 97.6893° |
| perigee height: | 523 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 183.4103° |
| argument of perigee: | 140.4009° |
| revolutions per day: | 15.03949181 |
| mean anomaly at epoch: | 220.0520° |
| orbit number at epoch: | 90697 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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