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 29499U 06044A 23334.48180653 .00004629 00000-0 59552-3 0 9997
2 29499 98.3810 39.4717 0192522 139.0211 284.7738 14.69432653891441
| Epoch (UTC): | 30 November 2023 11:33:48 |
| Eccentricity: | 0.0192522 |
| inclination: | 98.3810° |
| perigee height: | 527 km |
| apogee height: | 798 km |
| right ascension of ascending node: | 39.4717° |
| argument of perigee: | 139.0211° |
| revolutions per day: | 14.69432653 |
| mean anomaly at epoch: | 284.7738° |
| orbit number at epoch: | 89144 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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