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 23152.08176434 .00002952 00000-0 21372-3 0 9991
2 29507 97.6888 185.3949 0045220 133.7722 226.7260 15.03961917907225
| Epoch (UTC): | 01 June 2023 01:57:44 |
| Eccentricity: | 0.0045220 |
| inclination: | 97.6888° |
| perigee height: | 523 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 185.3949° |
| argument of perigee: | 133.7722° |
| revolutions per day: | 15.03961917 |
| mean anomaly at epoch: | 226.7260° |
| orbit number at epoch: | 90722 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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