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 23151.61603336 .00003037 00000-0 21975-3 0 9999
2 29507 97.6889 184.9318 0045186 135.3088 225.1793 15.03959387907205
| Epoch (UTC): | 31 May 2023 14:47:05 |
| Eccentricity: | 0.0045186 |
| inclination: | 97.6889° |
| perigee height: | 523 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 184.9318° |
| argument of perigee: | 135.3088° |
| revolutions per day: | 15.03959387 |
| mean anomaly at epoch: | 225.1793° |
| orbit number at epoch: | 90720 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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