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 22136.55571240 .00004925 00000-0 37598-3 0 9991
2 43017 97.6786 32.0485 0247886 292.4736 65.0400 14.81198444242399
| Epoch (UTC): | 16 May 2022 13:20:13 |
| Eccentricity: | 0.0247886 |
| inclination: | 97.6786° |
| perigee height: | 452 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 32.0485° |
| argument of perigee: | 292.4736° |
| revolutions per day: | 14.81198444 |
| mean anomaly at epoch: | 65.0400° |
| orbit number at epoch: | 24239 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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