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 39287U 13056C 22144.99449482 .00000921 00000-0 28934-3 0 9997
2 39287 49.5450 62.8819 5197583 272.3888 31.8461 5.24685856165024
| Epoch (UTC): | 24 May 2022 23:52:04 |
| Eccentricity: | 0.5197583 |
| inclination: | 49.5450° |
| perigee height: | 340 km |
| apogee height: | 14882 km |
| right ascension of ascending node: | 62.8819° |
| argument of perigee: | 272.3888° |
| revolutions per day: | 5.24685856 |
| mean anomaly at epoch: | 31.8461° |
| orbit number at epoch: | 16502 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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