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 39086U 13009A 22226.17233819 .00000022 00000-0 24450-4 0 9990
2 39086 98.5488 50.9552 0002322 93.9799 266.1650 14.32056509494740
| Epoch (UTC): | 14 August 2022 04:08:10 |
| Eccentricity: | 0.0002322 |
| inclination: | 98.5488° |
| perigee height: | 783 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 50.9552° |
| argument of perigee: | 93.9799° |
| revolutions per day: | 14.32056509 |
| mean anomaly at epoch: | 266.1650° |
| orbit number at epoch: | 49474 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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