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 43017U 17073E 22176.67998809 .00002140 00000-0 16427-3 0 9997
2 43017 97.6751 70.5380 0248983 160.5802 200.5108 14.81436198248332
| Epoch (UTC): | 25 June 2022 16:19:10 |
| Eccentricity: | 0.0248983 |
| inclination: | 97.6751° |
| perigee height: | 450 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 70.5380° |
| argument of perigee: | 160.5802° |
| revolutions per day: | 14.81436198 |
| mean anomaly at epoch: | 200.5108° |
| orbit number at epoch: | 24833 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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