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 15945U 85069B 22228.31213087 .00000284 00000-0 30903-4 0 9996
2 15945 82.5299 166.3784 0019729 171.9064 188.2474 14.84247707979689
| Epoch (UTC): | 16 August 2022 07:29:28 |
| Eccentricity: | 0.0019729 |
| inclination: | 82.5299° |
| perigee height: | 602 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 166.3784° |
| argument of perigee: | 171.9064° |
| revolutions per day: | 14.84247707 |
| mean anomaly at epoch: | 188.2474° |
| orbit number at epoch: | 97968 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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