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 39439U 13066Z 22179.46318331 .00002564 00000-0 30150-3 0 9993
2 39439 97.6368 152.8450 0063042 5.6165 354.5743 14.84288542463686
| Epoch (UTC): | 28 June 2022 11:06:59 |
| Eccentricity: | 0.0063042 |
| inclination: | 97.6368° |
| perigee height: | 572 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 152.8450° |
| argument of perigee: | 5.6165° |
| revolutions per day: | 14.84288542 |
| mean anomaly at epoch: | 354.5743° |
| orbit number at epoch: | 46368 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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