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 23151.88216544 .00003011 00000-0 21792-3 0 9998
2 29507 97.6889 185.1964 0045202 134.4274 226.0665 15.03960855907199
| Epoch (UTC): | 31 May 2023 21:10:19 |
| Eccentricity: | 0.0045202 |
| inclination: | 97.6889° |
| perigee height: | 523 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 185.1964° |
| argument of perigee: | 134.4274° |
| revolutions per day: | 15.03960855 |
| mean anomaly at epoch: | 226.0665° |
| orbit number at epoch: | 90719 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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