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 29522U 06050A 23088.49884479 .00000411 00000-0 23792-3 0 9997
2 29522 98.7587 103.0769 0010290 163.5534 196.5975 14.14219682846199
| Epoch (UTC): | 29 March 2023 11:58:20 |
| Eccentricity: | 0.0010290 |
| inclination: | 98.7587° |
| perigee height: | 837 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 103.0769° |
| argument of perigee: | 163.5534° |
| revolutions per day: | 14.14219682 |
| mean anomaly at epoch: | 196.5975° |
| orbit number at epoch: | 84619 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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